[ 3 / biz / cgl / ck / diy / fa / ic / jp / lit / sci / vr / vt ] [ index / top / reports ] [ become a patron ] [ status ]
2023-11: Warosu is now out of extended maintenance.

/sci/ - Science & Math


View post   

File: 54 KB, 800x419, ScrubX.png [View same] [iqdb] [saucenao] [google]
14853335 No.14853335 [Reply] [Original]

Previous: >>14848373

OH GUOOOD I'M SCROOOBIN' OOO

>> No.14853340
File: 105 KB, 959x722, Apu postimerkkeilijä.jpg [View same] [iqdb] [saucenao] [google]
14853340

>>14853335
FTS Archive
https://drive.google.com/drive/folders/1KCJBL632oieD1r6JOh_5Eg9NTcf_-hH8?usp=sharing

>> No.14853386

ded

>> No.14853410
File: 2.19 MB, 3105x3697, Firefly_Alpha_1st_Flight.jpg [View same] [iqdb] [saucenao] [google]
14853410

TWO WEEKS

>> No.14853418
File: 950 KB, 958x1196, rocketman.png [View same] [iqdb] [saucenao] [google]
14853418

Glass the earth, demigod war eventually

>> No.14853426

sfg is dead

>> No.14853460
File: 735 KB, 528x932, hop wen raptor.png [View same] [iqdb] [saucenao] [google]
14853460

Jay Leno at Starbase
https://www.youtube.com/watch?v=wluBlr1j4qk

>> No.14853467
File: 449 KB, 1028x1415, ns_display.jpg [View same] [iqdb] [saucenao] [google]
14853467

Im schwuasted and reposting anon post from last thread :) gnight boys im playin darts wirh a divorced guy (i fucjed his wife (((well technically she blowrd me but who's countin ahaha))))))

>> No.14853471

****(techmically ex wife ;)

>> No.14853487
File: 242 KB, 1200x900, Euclid_NISP_instrument.jpg [View same] [iqdb] [saucenao] [google]
14853487

soon

>> No.14853489
File: 9 KB, 200x313, mouse-under-water.jpg [View same] [iqdb] [saucenao] [google]
14853489

SpaceX should put a 20 meter telescope directly in front of JWST, using Webb as a secondary shield.

>> No.14853491
File: 173 KB, 560x420, boccry.gif [View same] [iqdb] [saucenao] [google]
14853491

>>14853319
don't pull my leg, I actually want to know

>> No.14853500
File: 323 KB, 1920x1080, sshot-098.jpg [View same] [iqdb] [saucenao] [google]
14853500

https://www.youtube.com/watch?v=wluBlr1j4qk

Internally SpaceX watches NSF live for their coverage lol

>> No.14853501

>>14853487
E wi hopefully find out when in November, with the ESA ministerial. Personally looking forward to Eucli finding the first quasars.

>> No.14853513

good morning spacecels
how's that moon base?

>> No.14853517

>>14852920
>>14852933
>>14852942
This is amazing. How is NASA actually doing something well?

>> No.14853526

>>14853513
Honestly, a south pole or far side lunar outpost would be incredibly gay because you couldn't check in on it from your backyard.

>> No.14853529

>>14853517
I'M...I'M GONNA SCROOOOOUB

>> No.14853544
File: 434 KB, 1536x2048, FXYIGBsaUAAxJu9.jpg [View same] [iqdb] [saucenao] [google]
14853544

So when's the next expected Artemis 1 attempt? They can't extend the certification for that emergency system thingy forever can they?

>> No.14853566

is it possible to see lights in the cities from the Moon

>> No.14853570

>>14853544
woah cat out of time

>> No.14853590

>>14853517
They've replaced the ones in charge of previous HLS picker with the Biden approved ones. We'll see

>> No.14853592

>>14853590
But that doesn't make any sense.

>> No.14853617

>>14853592
It does if you understand the timeline and the context where the original aware took place.

>Trump wants to go to the moon (away from Obama's Mars)
>Dems win congress
>Dems defund NASA's requested budget for HLS by allocating only 1/3 of the requested amount
>This achieves their desired goal of stopping Trump's goal of HLS
>Trump loses
>Biden wins
>NASA head admin resigns (as is tradition with new gov)
>Interm leads the decision making process without political heads involved
>Interm chooses Starship as winner
>Congress rage at (interm) NASA for choosing a HLS winner before Bill Nelson took his office
>Interm head picking Starship resigns
>Bill Nelson becomes head of NASA
>HLS manager gets demoted and removed from HLS program entirely
>Someone else gets chosen and placed at the helm

>> No.14853618

>>14853617
We were lucky

>> No.14853626

>>14853617
You forgot the part where they stop being shit and start being productive. You know, the part where it stops making sense.

>> No.14853630
File: 42 KB, 932x622, biden_02.jpg [View same] [iqdb] [saucenao] [google]
14853630

>>14853617
Biden is based

>> No.14853651

>>14853487
Euclid will probe the history of the expansion of the universe and the formation of cosmic structures by measuring the redshift of galaxies out to a value of 2, which is equivalent to seeing back 10 billion years in the past. The link between galactic shapes and their corresponding redshift will help to show how dark energy contributes to the increased acceleration of the universe. The methods employed exploit the phenomenon of gravitational lensing, measurement of baryon acoustic oscillations, and measurement of galactic distances by spectroscopy.

>> No.14853835

From recent Tweets it seems like SpaceX expects Raptor 2s to be less than completely reliable in the near to mid term.

>> No.14853854
File: 845 KB, 3000x2000, RS1 Flight 1 vertical 081322 (ABL Space) 2.jpg [View same] [iqdb] [saucenao] [google]
14853854

>>14853410
>reaches orbit first
nothin personnel kid

>> No.14853870

>>14853630
I miss 2018 when only one political faction used "based".
>>14853835
What tweets?

>> No.14853882
File: 188 KB, 1073x1073, 1648934496507.jpg [View same] [iqdb] [saucenao] [google]
14853882

non-chinese on the station when?

>> No.14853937

>>14853517
because Congress hasn't gotten involved yet?

>> No.14853959
File: 80 KB, 640x426, 1647456114836.jpg [View same] [iqdb] [saucenao] [google]
14853959

>nasa wants another moon lander
ok sure but who is viable?

>> No.14853969

>>14853959
>nasa wants another moon lander
NASA should be happy they get Starship to play with.

>> No.14853971

>>14853969
they are but they want redundancy

>> No.14853978

>>14853971
Meh, HLS has a malfunction, and elon mentions they already have 10 more out back with improved hardware.

>> No.14853983

>>14853971
A second Starship

>> No.14853986

>>14853971
They want endless contests and bidding, not a real mission. SLS will never launch, SLS can never end. HLS lander contract round 3 in 2024, coinciding with the restack and retest of the SRBs in anticipation of Artemis 1 (May She Never Fly, peace be upon the contractors, bless the senate amen)

>> No.14854002

>>14853971
No, they want regulatory capture. Aerospace is worth more than the world economy to any capture that escapes it and succeeds, which SpaceX is most likely in doing. Long after Elon dies, as long as the goal to put upwards of 100k people on the Moon or Mars happens, SpaceX goes from being a $125Bn to a $125T company. Tesla, alongside, will reach similar heights. Both his companies are set to completely diverge from traditional human history pathways. In doing so, they're all massive threats to existing bureaucracy, in that it will end the way politicians can line their pockets when private enterprise capability becomes light years ahead of government established methods. When SLS launches once every 2 years, at best, and throws away $3Bn of the $4Bn cost into the ocean every launch window, while SpaceX is launching to the tune of 100 SLS flights every 6 months and landing all of them, for less than the total cost of an entire SLS flight, the public begins to dangerously question the leadership capability of existing powers. It becomes impossible to not talk about it. Politicians then are forced to make long term decisions, for which, the payoffs they may never receive over short term decisions, for which the payoffs are always immediate and guaranteed.

It's all about how to maximize legalized bribery aka lobbying dollars.

>> No.14854057

>>14853526
>sky looker
>wants to ruin everything so he can look at the sky
No surprises here

>> No.14854061

>>14853630
based on animatronics

>> No.14854065

>>14854061
>technology
ngmi
Necromancy*

>> No.14854071

>>14853882
Not any time soon. One good thing they can claim about their half-a-century-late station is that they did it themselves (never mind their reliance on Russian technology). International cooperation would make it just a worse version of the current and future alternatives.

>> No.14854078
File: 418 KB, 1920x1080, firefox_2022-09-17_10-07-33.png [View same] [iqdb] [saucenao] [google]
14854078

This was a good one

>> No.14854083

>>14854078
https://www.youtube.com/watch?v=sBtYbn55dWA

>> No.14854086
File: 226 KB, 1920x1080, firefox_2022-09-17_10-09-54.png [View same] [iqdb] [saucenao] [google]
14854086

>> No.14854090
File: 203 KB, 1920x1080, firefox_2022-09-17_10-06-36.png [View same] [iqdb] [saucenao] [google]
14854090

>> No.14854098

>>14854078
Fineness Launch System is real

>> No.14854113

>>14853617
I hate politicians so much its unreal

>> No.14854120
File: 69 KB, 896x846, firefox_2022-09-17_11-10-52.png [View same] [iqdb] [saucenao] [google]
14854120

Feels good to see this shit in a current NASA document though

>> No.14854122

>>14854113
Reusable politicians was never envisioned for our nation's mission profile, we should transition to rapidly expendable politicians instead. One and done single use, then drop them into the sea when their term is up.

>> No.14854127
File: 1.34 MB, 3821x1911, FQtvx_ZXEAs98Lg.jpg [View same] [iqdb] [saucenao] [google]
14854127

> In the sustained phase, the HLS integrated lander will require the capability to dock to Gateway, land up to four crew members on the lunar surface for transfer to habitable lunar surface assets, operate for extended durations near the lunar south pole, and support eight-hour EVAs for the advancement of surface goals. Also, the agency has a goal of being able to perform two-crew sorties to non-polar landing sites

>up to 4 crew
>non-polar landings (possibly even far side)

LETS FUCKING GOOO

This is the NASA we all want

>> No.14854126

>>14854065
Thank you for pointing out my error

>> No.14854130

>>14854127
>transfer to habitable lunar surface assets
Hell yeah.

>> No.14854134
File: 31 KB, 913x430, firefox_2022-09-17_11-18-50.png [View same] [iqdb] [saucenao] [google]
14854134

>>14854130
Artemis Base Camp is insane

>> No.14854138
File: 763 KB, 1159x628, firefox_2022-09-17_11-21-53.png [View same] [iqdb] [saucenao] [google]
14854138

>6.5 days
>4 EVA's
>8+ hours per EVA

unff

and that's just the sortie missions

>> No.14854140

>>14853971
they want redundancy for SLS

>> No.14854154
File: 34 KB, 949x216, 2022-09-17_11-30-37.png [View same] [iqdb] [saucenao] [google]
14854154

They are gonna welcome the spaciousness of Starship HLS up there around the moon

>> No.14854156

>>14854138
Nice, very nice. Let's see DRM-H-002's visualization.

>> No.14854164
File: 640 KB, 1141x693, firefox_2022-09-17_11-33-33.png [View same] [iqdb] [saucenao] [google]
14854164

>>14854138
>>14854156
We'll get to that

>> No.14854165

>>14854154
I just realized that these astronauts are going to have the most spacious travel. Once space travel becomes more regular they're going to shove more people into Starship, so things will get more crowded as they advance.

>> No.14854167
File: 725 KB, 1140x636, firefox_2022-09-17_11-34-22.png [View same] [iqdb] [saucenao] [google]
14854167

>>14854164
>>14854156

>> No.14854169

>>14854120
Where can I get this document?

>> No.14854172

>>14854164
>>14854167
Everything post-Altair is so ugly I'm glad that Starship HLS will replace most of these reference designs

>> No.14854173
File: 1.39 MB, 1x1, Attachment+A01+ConOps_HLS-CONOP-006+Sustained+Phase+HLS+Program+ConOps_Revision_A.pdf [View same] [iqdb] [saucenao] [google]
14854173

>>14854169

>> No.14854175

If the moon had a breathable atmosphere and liquid surface water would it have developed life just due to proximity to Earth?

>> No.14854181

>>14854175
Maybe some panspermia when Earth got a particularly big impact, bigger problem would be keeping air/water on the lunar surface when all it wants to do is wisp away into space.

>> No.14854182

We will put life in Europa's oceans and see what happens

>> No.14854183

>>14854182
muh planppeary protectionns nooo you cant doo that nooo muh pristine scientific environoment

>> No.14854184

>>14854182
That's a really fancy way of saying "I'm gonna build an outhouse with a 5km shit tube."

>> No.14854190
File: 195 KB, 1024x1018, 1024px-Back_side_of_the_Moon_AS16-3021.jpg [View same] [iqdb] [saucenao] [google]
14854190

>>14854164
>The Non-Polar Sortie missions could land at sites within a wide range of latitudes and are not restricted to solely the Earth-facing side, which requires the HLS integrated lander to be capable of operating in a wide range of
surface thermal and solar angle environments.

NASA wants a human landing at the far side so bad I can sense it lmao, first humans to stand on a surface without Earth visible in any direction they look... what's the best location to land on?

>> No.14854193
File: 1.21 MB, 2000x944, tree-of-life_2000.png [View same] [iqdb] [saucenao] [google]
14854193

>>14854182
b-but that would cause a big new branch to form in the tree of life

>> No.14854197
File: 2.54 MB, 1920x1080, 1663064870250434.webm [View same] [iqdb] [saucenao] [google]
14854197

https://twitter.com/SciGuySpace/status/1571163692439322625
>One of the payload operators says the New Shepard-23 ballistic reentry reached 15 Gs during its return to Earth. At this force passengers would have passed out, but it probably would not have been fatal.
>15 Gs
>probably
OHNONONONO

>> No.14854205
File: 152 KB, 800x450, 1661518010885.jpg [View same] [iqdb] [saucenao] [google]
14854205

>>14854193
>sea scorpions
>trilobites
>ammonites
>armored fish
>extinct

>> No.14854217

>>14854205
once we introduce a few random species into Europa a biosystem beyond our wildest imagination will form

>> No.14854218

>>14854205
i miss them too

>> No.14854229

>>14853491
yeah it'd be 2g

>> No.14854230

>>14854197
Someone needs to go to jail for this

>> No.14854238

>>14853491
>>14854229 is right. 1g is normal. A rocket with 1g of thrust just hovers. But the crew still experience 1g since they're basically standing on a floating platform.

>> No.14854246

>>14854197
I saw the tweet and the first thing that came to mind was "Someone on /sfg/ is going to be going Oh No Bros No No No No."

I feel very comfortable in this relationship.

>> No.14854247

>>14853959
Just have Northrup Grumman build an apollo lem.

>> No.14854249
File: 48 KB, 961x276, firefox_2022-09-17_12-05-19.png [View same] [iqdb] [saucenao] [google]
14854249

>> No.14854250 [DELETED] 

>>14853292
>if you have a rocket whose engines can accelerate it with 2Gs launching off a planet with 1G surface gravity, the ship will accelerate at 1G. But how many will the crew inside experience? 3?
If a rocket is accelerating at 2g (20m/s/s) it's accelerating at 2g (20m/s/s) no matter what the planet's gravity is like. If the rocket engines are thrusting just enough so that the rocket can hover the rocket's acceleration is 0g (0m/s/s)

>> No.14854254

You fags will turn around on Gateway just you wait, will prove to be a vital and versatile staging ground

>> No.14854257 [DELETED] 

>>14854250
A hovering rocket is under 1g load

>> No.14854258 [DELETED] 

>>14854250
to add to that if the rocket is accelerating vertically at 5 g an accelorometer internal to the rocket will measure 5 g + the value of acceleration that bodies in freefall experience on that planet

>> No.14854264

>>14854197
15 Gs can be lethal and fatal for the passengers BO has flown. Some of which are not physically fit at all.

>> No.14854268
File: 2.85 MB, 2048x1536, Mars_Perseverance_ESF_0042_0670681765_127ECM_N0031392EDLC00042_0010LUJ.png [View same] [iqdb] [saucenao] [google]
14854268

>> No.14854271
File: 34 KB, 986x268, firefox_2022-09-17_12-14-27.png [View same] [iqdb] [saucenao] [google]
14854271

So much different from Apollo

>> No.14854272

>>14854268
landing the sample return helis will much simpler.

>> No.14854279

>>14854264
It would have killed Shatner 100%.

>> No.14854282

>The HLS integrated lander will have the capability to land automatically without crew on board

>> No.14854284

>>14854057
I don't want those lazy, inevitably EARTHER contractors sitting around on their asses wasting my tax dollars. They need accountability and constant monitoring, similar to small children or a retarded dog.

SpaceX I trust to build a base wherever idc.

>> No.14854286

>>14854264
For comparison, Crew Dragon abort accelerates away at 3.3Gs

Tesla Plaid does ~1.3Gs and some people already feel like they're seeing white lights at that acceleration

15Gs are insane. Some humans have shown on record to survive, but its rare.

You can pass out at 3.6g easily.

https://www.youtube.com/watch?v=DMKcO-T5Y4o

>> No.14854290

>>14854254
It only exists because SLS is too underpowered to get to the lunar south pole on its own so rendezvous with orion and HLS could never happen in earth parking orbit, and it is only supported because it’s a freak show of expensive parts that have already begun fabrication so now congress can’t cancel it thus it provides political stability to Artemis. Nothing about it is “cool” other than the fact that SLS is so gay it doesn’t have the cadence to launch it so now SpaceX is giving it a hitchhike with the FH

>> No.14854291

>>14854282
Why would it do that? If you're landing cargo you still need someone there to unload boxes of shit.

>> No.14854295

>>14854290
It will be the ISS of the moon

>> No.14854298

>>14854291
Unloading can be automated, done remotely, or by someone who arrived on another lander.

>> No.14854301

>>14854295
>pressurized volume: 123 m^3
>only manned one month every 2 years
yeah okay fag

>> No.14854305

>>14854301
I seriously doubt it, NASA will seek to expand beyond just SLS Orion

>> No.14854306

>>14854197
This is very misleading and disgraceful reporting by Eric Berger. Crewed launches have more mass so g force would be much less.
Eric should stop posting retarded tweets.

>> No.14854307

>>14854217
>>14854182
I can't wait, do it do it I wanna see what happens, how many whales and sharks and squid can starship hold?

>> No.14854311

>>14854298
>or by someone who arrived on another lander.
That one seems more likely, automating unloading with robots sounds like a massive waste of time. Even with the HLS Starship using the higher-up engines to land, astronauts are still gonna have to shelter when a lander comes down.

>> No.14854313
File: 105 KB, 612x491, Confused Apu.png [View same] [iqdb] [saucenao] [google]
14854313

>>14854197
But that webm clearly says "Zero-G"

>> No.14854314
File: 46 KB, 943x308, firefox_2022-09-17_12-27-51.png [View same] [iqdb] [saucenao] [google]
14854314

NASA's got the right idea

>> No.14854315
File: 66 KB, 550x413, blue-origin-new-shepard.jpg [View same] [iqdb] [saucenao] [google]
14854315

your encapsulet bro

>> No.14854319

>>14854307
thousands in larvae form

>> No.14854320

>>14854286
>>14854197
Thats the crazy part. If BO has been flying passengers with 15Gs as their abort acceleration, then thats an issue. BO really needs a safety threshold and redesign their safety systems. They're essentially flying without any reliable safety systems. Death can easily happen at this type of operational procedures.

>> No.14854325

>>14854254
>we need a space station to get to the moon!
>why? we didn't back in the 70s
>because it's an important stepping stone to mars

Gateway exists because some compete retards in NASA wanted to include a trial run Mars mission habitat in the lunar program. Artemis III isn't going to be using Gateway for its mission. There's no reason why we need a lunar station but the same faggots who think that SLS and Orion are going to be vital parts of the Mars exploration are still allowed to provide input for mission designs.

>> No.14854326

>>14854314
anon I really appreciate you doing the reading for rest of the class
I still wish we didn't have to depend on NASA, wish some private company did it by themselves. Just say the coords and pay and boom.

>> No.14854330

Why does Orion cost so damn much

>> No.14854333

>>14854330
after re-use post Artemis IV it will be cheaper

>> No.14854336

>>14854330
It's been in development since George W Bush was President.

>> No.14854340

>>14854320
15G at the peak. We don't know for how long those forces were sustained. Even old people can take some pretty high accelerations provided the period is short enough.

>> No.14854350

>>14854340
This guy in the video >>14854286 here passed out in a second at 3.6G. He's a healthy adult in his early-mid 30s when the video was made.

At 15G, if you're over the age of 60, you'd pass out and probably die of brain aneurism/heart attack/etc. The abort engine firing seems to have lasted atleast 20 seconds, so thats a long time.

>> No.14854364
File: 46 KB, 1046x313, firefox_2022-09-17_12-45-06.png [View same] [iqdb] [saucenao] [google]
14854364

HLS disposal strategy

>>14854326
its some damn good reading, I wont be reading the rest of the docs just this one, the only interesting one

>> No.14854366

G force should be easy to calculate based on telemetry.
Sustained 15g for 20 seconds is mathematically impossible.

>> No.14854367

>>14854330
Because the purpose of Orion is to cost as much as possible.

https://youtu.be/5OWUsMfCVWY

>> No.14854373

Morning, /sfg/.

>> No.14854374
File: 49 KB, 1065x503, firefox_2022-09-17_12-50-31.png [View same] [iqdb] [saucenao] [google]
14854374

Interesting contingencies

>> No.14854375

>>14854366
the capsule is tumbling and spinning

>> No.14854376

>2022
>still cant rent space on a space station
>cant even rent space on a satellite
dark timeline

>> No.14854380

>>14854330
Materials-wise it's probably average for going-to-space missions
After that is when things start getting crazy: because it's aerospace every single part installed has a paper trail from the time it is made to the time it is installed
Since it's purpose-built it also amortizes its R&D cost across every planned unit
Because it is manned, that R&D cost is not cheap
And then, after all of that is said and done, it gets marked up to whatever acceptable profit margin they got in negotiations

>> No.14854383

>>14854376
>>cant even rent space on a satellite
wdym, you can rent bandwidth on a satellite. That's how blockstream streams the bitcoin blockchain.

>> No.14854388

>>14854374
>single crew capability to operate and fly the vehicle
Goddamn that's fucking radical. Imagine being the lone astronaut piloting your very own Starship. Imagine waking up to absolute peaceful solitude every day of the drift towards Mars. Damn.

>> No.14854396
File: 646 KB, 1x1, Attachment+A01+ConOps_HLS-CONOP-007_HDL+CONOPS_Revision_A.pdf [View same] [iqdb] [saucenao] [google]
14854396

>The Human-class Delivery Lander (HDL) Concept of Operations (ConOps) describes the general
concepts associated with the delivery of large Cargo that either remains integrated with the HDL
on the Lunar surface, or that is offloaded from the HDL. The HDL is not intended to deliver crew.
The HDL and Cargo will be launched by the HDL provider’s procured launch vehicle(s) (LV), and
the HDL will be expected to perform complete delivery to the surface. Providers may choose any
approach to launch, aggregation, or staging architecture within the bounds of the HDL’s and the
Cargo’s operational and environmental limits.

>> No.14854405

I *still* don't understand why we need SLS + Orion for Artemis when we have Starship.
Can't we just use Starship + HLS and
Starship + 2nd lunar lander?
Or New Glenn + 2nd lunar lander.
Why SLS?

>> No.14854412
File: 58 KB, 1021x575, gE2Zc.png [View same] [iqdb] [saucenao] [google]
14854412

>>14854350
The escape motor wouldn't have produced 20 seconds of 15G acceleration. SRBs never produce constant acceleration like that. Here's a thrust vs. time graph for the Titan IV SRBs. Most solids have a burn pattern that looks something like this.

That guy in the centrifuge is also sitting in a different pose from the passengers on New Shepard. His head is at the top with the acceleration pushing down towards his feet. This makes sense for that centrifuge since it's RAF hardware and needs to simulate the kinds of things fighter pilots would be expected to encounter. Crewed rockets have the acceleration vector running backwards through the chest rather than downwards along the spine which lets you tolerate higher G loads for longer.

I'm not saying it'd be a pleasant experience but thinking that the abort motor would automatically cause every old on board to stroke out and die is misunderstanding the forces at play.

>> No.14854416

>>14854405
It is mandated by law. The law is decided by the Senate. The Senate has vested financial interests in SLS continuing production. Therefore, we must arrest the entire Senate for money laundering.

>> No.14854419

>>14854416
reported to Jan 6. Committee

>> No.14854422
File: 791 KB, 1104x664, firefox_2022-09-17_13-05-42.png [View same] [iqdb] [saucenao] [google]
14854422

>> No.14854425
File: 757 KB, 1288x638, firefox_2022-09-17_13-06-48.png [View same] [iqdb] [saucenao] [google]
14854425

>> No.14854430

>>14854405
To be fair, we don't "have Starship." Starship is in development but it's a long way from being real. And if shit goes down and SpaceX goes bankrupt, Starship just evaporates like a dream at sunrise.

>> No.14854435

>>14854422
Pretty sure that's a screenshot from KSP.

>> No.14854439

>>14854430
if Starship evaporates then Artemis 3 is no-go.
The next HLS will be build by... 2028? 2030? We were supposed to go to Mars by then..

>> No.14854445

>>14854439
it's over....

>> No.14854446

>>14854412
One might add that it was positive Gs (probably the 15) during the initial abort and then hard negative Gs while the motor was still firing. The drag in the transonic regime quickly overpowered the thrust.

>> No.14854450
File: 85 KB, 1600x900, Britney_Spears_be_like-3228073918.jpg [View same] [iqdb] [saucenao] [google]
14854450

>>14854374
>and crew exposure to toxic
???

>> No.14854453

>>14854450
The only song that can incapacitate a crew...

>> No.14854456
File: 417 KB, 1000x600, Phil-Mason-2019.png [View same] [iqdb] [saucenao] [google]
14854456

>>14854405
Listen muskcuck, Starship is a fake, a phony, a fraud. it's bascally the same technology nasa had in the 50s. space-x is barely slowly crawling back to parity with stale nasa tech. ever heard of dcx? redstone? yeah, that's falcon9. starship is a bigger dcx, except nasa dcx worked and starship crashed about 10 times. i know which one i put money on

>> No.14854459
File: 53 KB, 1024x209, firefox_2022-09-17_13-13-26.png [View same] [iqdb] [saucenao] [google]
14854459

love how low lovely Earth will be on the horizon

>> No.14854464

new ONIONS just dropped
https://www.youtube.com/watch?v=nzplxkfPdEA

>> No.14854468

>>14854464
Can you check if Thunderf00t has any new SpaceX takedowns? I think /sfg/ needs a reality check

>> No.14854472
File: 717 KB, 1559x748, firefox_2022-09-17_13-19-05.png [View same] [iqdb] [saucenao] [google]
14854472

1080p live stream video during EVA LETS GOOO

>> No.14854476

>>14854472
>1080p in 2026
the average person will have 8k by then

>> No.14854477

>>14854476
space always lags behind, ISS just got UHD 4 years ago

>> No.14854478

>>14854472
Wifi on the fucking moon. Can we just take a moment?

>> No.14854481

>>14853630
Based at sniffing kids.

>> No.14854483

>>14854476
>the average person will have 8k by then
you're probably mistaken
4k at most. we've been at 1080p for many years, it's just not that much of an improvement for quadratically more work

>> No.14854484

>>14854472
>>14854478
Look into a company called Aquarian Space
I still think the lunar market is 10 years too early but people are jumping into shit like that now

>> No.14854485

>>14854430
US military won't allow Space X to go bankrupt, they are in the MIC club now

>> No.14854486
File: 1.42 MB, 4800x2700, HLSSS.jpg [View same] [iqdb] [saucenao] [google]
14854486

>>14854472
>HLS mounted cams
>2k radius for non-LTV surface ops
>Starship HLS is 120m tall

hooooly shhiiitt, imagine the views from that thing, giving a wide overview of the whole LZ area, SpaceX better not skimp out on the HLS cams

>> No.14854488

>>14854472
1080p at 15fps

>> No.14854493
File: 225 KB, 1188x892, firefox_2022-09-17_13-27-35.png [View same] [iqdb] [saucenao] [google]
14854493

>>14854472

>> No.14854494

>>14854254
I'm expecting gateway to morph in to the ISS succesor anyway in the future.
ISS is going to be deorbited in the next decade and it's just more logical to have a new spacestation at the moon as support to moon missions.

>> No.14854495

>>14854483
you mean we've been at 4K for many years

>> No.14854498

>>14854494
Yep, NASA wants to hand off LEO to commercial space as soon as they possibly can, then they can fully focus their efforts on lunar and moon, the more assets they have there the harder it is to kill politically, Gateway practically guarantees the moon

>> No.14854500

>>14854498
lunar orbit*

>> No.14854503

>>14854493
>>14854472
Just think of the sheer difference in total data sent from Moon to Earth during all of Apollo, and then during Artemis III.

Artemis III total data stream will probably be 2x that of the entire Apollo 10-17 missions

>> No.14854508

>>14854486
>Starship HLS is 120m tall
what did he mean by this

>> No.14854510
File: 109 KB, 949x854, firefox_2022-09-17_13-35-54.png [View same] [iqdb] [saucenao] [google]
14854510

>>14854493
So much landing criteria

>> No.14854515

lunar deep drill cores wen?
lunar prospecting wen?
lunar oil exploration wen?

>> No.14854516

>>14854515
Locating, exploring and settling lunar lava tubes wen

>> No.14854518

Artemis time tables are already so fucking bad and, without a doubt, everything will need to be pushed back 4-5 years. Everything feels like a huge black pill

>> No.14854519
File: 330 KB, 950x800, B3M-SONIQAEqmLh.png [View same] [iqdb] [saucenao] [google]
14854519

>>14854508
>Starship is as tall as a wind turbine
>Starship is 35 stories tall

Starship is big!

>> No.14854520

>>14854519
>>14854508

>> No.14854527
File: 986 KB, 1221x663, firefox_2022-09-17_13-41-46.png [View same] [iqdb] [saucenao] [google]
14854527

>>14854518
NASA isn't making it any easier on themselves or HLS or the astronauts which such restrictive and challenging conditions compared to a simple equatorial landing

>> No.14854531

>>14854134
>>14854127
>>14854138
HLS Starship has enough volume to support up to 25 people on the Moon for arguably a full 3 months or more with stored mass within the pressurized area alone, and up to another 3 months via the unpressurized cargo section. NASA is being hyper conservative with 4 crew, in part, because Orion can hold a maximum of 6 people. Effectively sending 6 people to the Moon per launch for the next 10-15 years is painfully slow.

>> No.14854532
File: 697 KB, 1183x856, firefox_2022-09-17_13-43-08.png [View same] [iqdb] [saucenao] [google]
14854532

>>14854527
Its gonna be a challenge from the very first lunar return

>> No.14854540
File: 96 KB, 1089x629, firefox_2022-09-17_13-44-46.png [View same] [iqdb] [saucenao] [google]
14854540

NASA keeping the final location a guarded secret lmao

>> No.14854541

>>14854472
they WILL fuck this up

>> No.14854542

>>14854154
If HLS Starship was to be docked to the gateway, its going to be such a joke having a 165 foot tall hotel docked to basically a camper van. I suspect that astronauts will spend more time in the HLS Starship when docked to gateway and only move over to the gateway for when science needs to be done or they need to communicate with mission control through the high gain antenna or w/e. Though, with the way HLS Starship will be built, its basically Gateway 5.0 and can do everything it can and more.

>> No.14854543

>>14854540
They really don't want to give the Chinese a chance to preempt their landing site, do they

>> No.14854548
File: 675 KB, 2400x1350, artemis-iii-landing-regions.jpg [View same] [iqdb] [saucenao] [google]
14854548

>>14854543
Not one bit lmao, it will be within 6 degrees of the South Pole, and one of these locations, and thats all we get till the astronauts are in orbit

>> No.14854549

>>14854531
We don’t know the final volume of HLS moonship do we? Unless it’s been published, I wouldn’t be surprised if the interior is heavily modified from what Musk has been implying for base SS with NASA allocating a lot of space for cargo and science equipment with only an airlock and a few rooms for actual astronaut space. If orion is limited to ~4 astronauts, then that is your bottleneck and you will design HLS starship around that

>> No.14854550

>>14854472
>5ghz
why? do 2.5 get better range and plenty throughput

>> No.14854552
File: 571 KB, 1920x1080, Starships double-teaming Gateway.jpg [View same] [iqdb] [saucenao] [google]
14854552

>>14854542

>> No.14854556
File: 344 KB, 863x517, Screenshot 2022-09-17 114700.png [View same] [iqdb] [saucenao] [google]
14854556

https://www.youtube.com/watch?v=nzplxkfPdEA
>Miranda engine will be tap-off
>8% higher thrust on 2nd Alpha flight, other performance increases coming
otherwise this isn't worth watching

Also, is Estronaut stuck in California with Firefly if SLS makes another attempt? It crossed my mind after the second scrub as a possibility, but now the dates are aligned.

>> No.14854558

>>14854543
Artemis would have to suffer some significant delays for China's 2030 landing date to be able to get there first. Artemis I would have to explode on launch for them to have a real chance.

>> No.14854559

>>14854548
r0lling

>> No.14854560
File: 48 KB, 320x444, science.jpg [View same] [iqdb] [saucenao] [google]
14854560

>>14854552
>two weeks

>> No.14854561

>>14854556
LMAO

>> No.14854562

>>14854556
higher chance for SLS to scrub.
>>14854550
It's that easy when you have no noise

>> No.14854563

>>14854264
>>14854279
On average, the age of Blue Origin's passengers have been 40-50+. If Bezos had been on this flight, for example, good chance he would be in the ER right now--he might have even died. 15G is absolutely insane. 15G is 1.5x the amount of g-forces experienced by a capable pilot conducting aircraft maneuvers in an F-22 at supersonic velocities. And these people are in specialized suits AND are trained for it, and can still black out from it. Untrained travelers, many of whom who are in their 50s and 60s will die if they experienced it.

>> No.14854567

you all are too bitchy about 15 g. It only lasts a few seconds and shuffles the blood around and that's it.

>> No.14854568

15 g what are you talking about 10 g they clearly only experienced 8.5 g during abort the g monitors show it clearly at 5 g the passengers would have been completely fine at the 3 g's the capsule experienced on safe abort

>> No.14854570

>>14854527
NASA being over-ambitious is one of the few great things about the Artemis landings

>> No.14854571

>>14854558
>Artemis I would have to explode on launch for them to have a real chance.
not out of the question. Granted even the 5DY seems to be in design limbo. Anyone with interest in the moon is going at a snail’s pace

>> No.14854573

>>14854570
Yeah for real, and Starship HLS matches that ambition

>> No.14854574
File: 1.73 MB, 1944x2592, IMG_20150325_140942.jpg [View same] [iqdb] [saucenao] [google]
14854574

>shrugs off 46 g
Pussies

>> No.14854577

>>14854574
Stapp was in a league of his own, man could probably ride an SRB to orbit on top

>> No.14854578
File: 13 KB, 579x491, firefox_2022-09-17_13-59-03.png [View same] [iqdb] [saucenao] [google]
14854578

rereeeeeee i hate being a normiee

>> No.14854579
File: 61 KB, 1294x794, outer solar system.jpg [View same] [iqdb] [saucenao] [google]
14854579

this is pretty cool

>> No.14854580

>>14854578
just order a FOIA bro

>> No.14854584
File: 137 KB, 1080x1320, starship of liberty.jpg [View same] [iqdb] [saucenao] [google]
14854584

>>14854519
>>14854486
Statue of Liberty is 93 meters tall fully stacked, but 46 meter on top of the base.
Starship stacked is 120M, 50M with just Starship.

>> No.14854588
File: 3.55 MB, 2953x2050, FU40-ziUsAApTVq.jpg [View same] [iqdb] [saucenao] [google]
14854588

>>14854584
i got a better

>> No.14854590

>>14854573
I would even argue NASA wouldnt be so bold without SpaceX and Starship. It shows a surprising amount of confidence on their part. I can't quite remember who I heard it from, but some insider expects Artemis to "evolve" once landings get underway, both in terms of base camp expansion and competing BLEO crew launch (marketed to congress as redundancy to SLS), eventually replacing SLS/Orion with commercial options

>> No.14854591

>>14854590
Fuck that would be awesome, we have a lot to make up for loitering 40 years in LEO

>> No.14854592

>>14854567
If I did it, I would go to prison. But when Bezos does it? You clap

>> No.14854593
File: 74 KB, 899x918, firefox_2022-09-17_14-05-36.png [View same] [iqdb] [saucenao] [google]
14854593

This one is interesting too

>> No.14854597
File: 1.54 MB, 1x1, Attachment+A5_HLS-VV-002+HLS+Integrated+Lander+Verification+Guidebook+-+Sustained+Phase_Rev+A.pdf [View same] [iqdb] [saucenao] [google]
14854597

>>14854593

>> No.14854596
File: 44 KB, 298x492, 1620576557058.jpg [View same] [iqdb] [saucenao] [google]
14854596

>>14854197
There's no way to sugarcoat this.

>> No.14854598

>>14854472
>>14854493
>SpaceX as part of demo1 HLS to the moon (uncrewed), adds a Starlink cargo/launch port to the vehicle
>adds 6 Starlink Gen2 satellites to HLS, sacrificing 15T from any notional payload NASA wants
>HLS Starship gets to the moon, during descent, it pauses in a specific lunar orbit, and launches 1 satellite every 30-45 seconds
>then descends to target
>each Gen2 Starlink satellite is expected to support up to 60Gbps bandwidth
>for a total of 360Gbps bandwidth across a 5-750km surface area per satellite
>there's now coverage across the dark side of the moon as well
>gen2 satellites will be configured to talk with gateway
>demo2 HLS arrives
>descends to a specific lunar orbit, orients itself facing the poles
>launches another 6 Gen2 satellites
>for another 360Gbps coverage and support
>all HLS Starship spacesuits come with 4K60Hz mounted cams and 8K60Hz with multi-spectral capability science cams
>all suits are capable of talking with an overhead Starlink satellite
>all suits are capable of independent live streams
>all SpaceX rovers are capable of similar optionalities
>all suits will have their own twitter accounts
>astronauts can at any time tweet from the moon, take selfies, and post clips of what they're doing or looking at in the form of a picture or video
>NASA's panties are soaked
>every other aerospace company in HLS is seething

>> No.14854600
File: 112 KB, 888x921, firefox_2022-09-17_14-08-35.png [View same] [iqdb] [saucenao] [google]
14854600

>>14854593
>>14854597
This is the real nitty gritty

>> No.14854603

>>14854571
That's why I'm not completely ruling it out. If Artemis II has to be a do over like OFT-2 was, then we might have a race, but probably not even then. The 5DY could be built a lot quicker than the LM-9, but there just isn't any real political will in Beijing to build a moon rocket, even one that doesn't require the design of new engines or 10m tooling. 2030 is still a very optimistic date for China.

>> No.14854604

>>14854173
>>14854396
>>14854597
link to this >>14854578 complete list of documents please

>> No.14854610
File: 74 KB, 680x383, bezos-head.png [View same] [iqdb] [saucenao] [google]
14854610

>>14854350
>>14854563
It doesn't matter if they pass out because they aren't piloting the rocket.

>> No.14854615
File: 46 KB, 640x618, 1661454597299453.jpg [View same] [iqdb] [saucenao] [google]
14854615

>>14854610

>> No.14854625
File: 1.05 MB, 2415x3000, S-IC_engines_and_Von_Braun.jpg [View same] [iqdb] [saucenao] [google]
14854625

>>14854588
If you've never seen an F1 engine in person, please anons make pilgrimage. It's not the most advanced engine ever, but the sheer size and brutal nature of it impressed me in a way few things have. An object so simple in purpose, made to do one thing only, and performing its mission admirably.

>> No.14854627
File: 1.60 MB, 2592x1944, IMG_20150325_141839.jpg [View same] [iqdb] [saucenao] [google]
14854627

>>14854625
It's true, they're so fucking big.
Pic related, Alamogordo NM

>> No.14854631

>>14854604
well fuck you too guys https://sam.gov/opp/69caee776b304322a256acd0b5deaf57/view#attachments-links

>> No.14854633
File: 376 KB, 1272x1967, space coomer.png [View same] [iqdb] [saucenao] [google]
14854633

>>14854598
I'm gonna need a new tissue box

>> No.14854635
File: 451 KB, 963x1960, 2022-09-17 14.23.33 cdn.arstechnica.net 8b811c79a45d.jpg [View same] [iqdb] [saucenao] [google]
14854635

>>14854549
You can fairly argue that the usable habitable volume for the HLS Moonship will be ~40% more than the total usable volume of the ISS. That's a reasonable estimate on the high side and ~25% more total usable volume of the ISS on the low side. Either way, its massive. And that's independent of the storage volume of the dual redundant airlocks AND, AND; the unpressurized cargo volume BELOW that (but above the fuel tank/batteries), which is expected to hold up to 50-100T of additional cargo. The Moonship is 9 meters across, that's 27 feet. For context, your living room on average is about 20 feet long, add the kitchen to that and you're at around 33 feet. So from your front door to halfway into your kitchen is how wide the Moonship physically is.

Let's assume that a solid two feet of space is going to go into setting up the walls, kevlar reinforcement material, electrical, pipes for fluid of various types, and general purpose system hardware. So from 27 feet you drop down to 25 feet. Then from your front door to 1/4th of the way into the kitchen. That's how wide is the usable volume. Next, remove about 6 feet of space from the center of that for the central column/tube by which astronauts move up and down through the decks. That gives you 9.5 feet on either side of the tube as usable space. An average bathroom is about 9-10 feet wide. So if you walk into any bathroom, from the door all the way to the shower wall is how much space in depth you have. Now circumference that and that's the usable volume horizontally. Each ring segment of the Starship is 3 meters tall, which is 9 feet. Which means each deck is 9 feet tall. Let's assume that each deck will lose about 1 feet in depth for electrical, pipes, general purpose hardware, and storage.

The ceiling of each deck is going to be 8 feet. Average ceilings in houses are about 8 feet, so each deck is as wide as a bathroom that wraps around the central column and the Moonship has 8 core decks. Huge useful space.

>> No.14854637

>>14854627
That's missing most of the bell

>> No.14854642

>>14854637
True, even without it it's still fuckhuge though. I wonder why that museum removed the bell, or maybe NASA did before donating it? Seems it'd be more impressive to leave it uncut.

>> No.14854646

>>14854642
Americans cant stand uncut things. Thats why they had to remove it.

>> No.14854652

>>14854598
>>every other aerospace company in HLS is seething
kek. I'd like to see them provide even 1/3rd of what Starship HLS can

>>14854604
https://sam.gov/opp/846a06fdcf3e408fa84ab6ac93b8cdc8/view

>> No.14854654

>>14854631
Wrong one

>>14854652
Original Published Date: Sep 16, 2022 03:00 pm CDT

>> No.14854655
File: 21 KB, 466x419, 2022-09-17 14.30.54 www.omnicalculator.com 1be9eb340725.jpg [View same] [iqdb] [saucenao] [google]
14854655

>>14854635
https://www.omnicalculator.com/math/cylinder-volume

1. 8 decks at 3m height per deck = 24m height
2. 4.5 meter radius = 9 meter diameter
3. Total usable cubic volume as a result of the calculation is pic related: 53,918.93 cubic ft.

Now, we're going to subtract 1/2 a meter from the height of each deck and 1/2 of a meter from the radius for all the space that will be lost for walls, supporting hardware, and storage. Which means our new variables are:
1. 8 decks at 2.5m height = 20m usable height
2. 4m radius = 8m usable diameter
3. Total usable cubic volume as a result of the calculation then is: 35,502.18 cubic feet.

According to this site: https://www.atobmoving.com/movesize.html, a 5 bedroom house is approximately 1300 cubic feet. That means, each Starship has a total usable volume (this time including the dual redundant airlocks AND unpressurized cargo area) of 27 5 bedroom houses. Let's assume that this math is too generous and drop that by 50%. That still means that the Moonship will have the equivalent space of 13.5 x 5 bedrooms worth of volume. That's absolutely nuts. Starship is such a game changer, it makes every other lander ever built and arguably to be built in the next 20 years by anyone else, a complete nonstarter. You have more usable space in a single Moonship than all of apollo capsules, lunar landers combined and maybe even all space shuttle launches with their crew sections added in.

>> No.14854657

>>14854627
this doesn’t do it justice. The Saturn V at JSC is ball numbingly large and it’s almost comical to see the fuckhuge engines and a giant rocket spanning the entire breadth of the hangar only to then see the small little Apollo capsule at the very end. So much energy for such a small little space craft just to reach our own natural satellite

>> No.14854658

>>14854652
>>14854654
Oh I see thank you. Had it all unzipped and organized already too

>> No.14854662
File: 82 KB, 789x913, firefox_2022-09-17_14-45-16.png [View same] [iqdb] [saucenao] [google]
14854662

gotta love how NASA operationalizes the fuck out of simple manual tasks

>> No.14854668

>>14854662
If you're going to hire people like Boeing to make a lander, every single thing it needs to be able to do needs to be explicitly in writing or they will either not do it or charge you a shitload to change the spec

>> No.14854670
File: 62 KB, 931x613, firefox_2022-09-17_14-49-34.png [View same] [iqdb] [saucenao] [google]
14854670

lmao at the last sentence

>> No.14854678

>>14854668
Alternately (and because NASA is legally banned from assisting China's space program in any material way), because these documents are meant to be public this could also be NASA's way of telling CNSA that they need a lander capable of at least this much if they plan to send taikonauts to the lunar surface

>> No.14854680
File: 66 KB, 923x858, firefox_2022-09-17_14-56-10.png [View same] [iqdb] [saucenao] [google]
14854680

NASA astronaut training insight

>> No.14854683
File: 78 KB, 1014x674, firefox_2022-09-17_14-57-40.png [View same] [iqdb] [saucenao] [google]
14854683

>>14854680

>> No.14854689
File: 118 KB, 960x1441, Page-from-Apollo-16-astro-001.jpg [View same] [iqdb] [saucenao] [google]
14854689

>>14854662
It happens

>> No.14854692

>>14854689
Modern NASA would never

>> No.14854698

>>14854598
>each Gen2 Starlink satellite is expected to support up to 60Gbps bandwidth
Wrong. Starlink Gen1 was supposed to do ~20Gbps. Musk said Gen2 has ~10x the bandwidth capacity, so that's 200 Gbps per Sat.

>> No.14854714
File: 958 KB, 1678x923, firefox_2022-09-17_15-12-27.png [View same] [iqdb] [saucenao] [google]
14854714

Swamp Works does some cool shit

>> No.14854717

>>14854714
They got a broad mandate and were set loose on blue-sky R&D, ya love to see it

>> No.14854719

>>14854717
That's one of the best things NASA can do, one of the things they are best equipped to do

>> No.14854726

>>14854543
>>14854548
They should announce it, let the Chinese land there, then use that as an excuse to scale up 10x what they were originally going to do.

>> No.14854727
File: 1.32 MB, 1671x891, firefox_2022-09-17_15-25-36.png [View same] [iqdb] [saucenao] [google]
14854727

cool shit from Stennis ASL

>> No.14854728

>>14854078
Sorry Ken not going to watch your video.

>> No.14854729

>>14854579
>super teeny tiny barely visible orange ring attached to the Sun
>that's actually the orbit of Mars

>> No.14854730

>>14854728
Whose Ken?

>> No.14854731

>>14854727
>They're building a Killdozer for the moon
praise him

>> No.14854732

>>14854731
BEAST is gonna be awesome, can't believe NASA is doing shit again

>> No.14854733

>>14854325
Why are you talking like a peasent squabbling with his wife about how they can't afford another outhouse, you are talking about the greatest and wealthiest and most advanced nation in world history, it shouldn't be a question of moon base or mars base, or you not thinking moonbase would be cool because it's uneeded for mars. Humans should put a base/s on the moon simply because it would be cool, they should be able to by now, they put buildings every where else why wouldn't one on the moon be cool, useful, helpful.

>> No.14854738

>>14854730
The guy who runs that youtube channel, he was recently whining on twitter about how his view count is way down and didn't want to believe he was riding the wave of excitement from the Starship hop tests.

>> No.14854740
File: 70 KB, 845x590, firefox_2022-09-17_15-32-48.png [View same] [iqdb] [saucenao] [google]
14854740

Jesus

>> No.14854741

>>14854740
:(

>> No.14854744

>>14854738
Ah well he only has 18k subs thats like nothing in modern youtube terms he;s at the mercy of the algo, at least this video is genuinely good so of course it will go ignored

>> No.14854746

>>14854405
>I *still* don't understand why we need SLS + Orion for Artemis when we have Starship.
SLS is at least based on a rocket that has been to orbit
Starship hasn't flown more than half way to orbit I don't think

>> No.14854747
File: 74 KB, 806x761, firefox_2022-09-17_15-37-54.png [View same] [iqdb] [saucenao] [google]
14854747

Everything so meticulously planned no wonder Skylab rebelled

>> No.14854751

>>14854740
That's what we like to call foreshadowing.

>> No.14854770

>>14854486
Will there be rovers with HD cams that just film themselves exploring the surface? How nice would that be going along for the ride with them visually

>> No.14854776

>>14854770
Don't see why NASA wouldn't put that on their LTV

>> No.14854784
File: 424 KB, 2173x1640, Astronaut Group 2 - S62-6759.jpg [View same] [iqdb] [saucenao] [google]
14854784

https://en.wikipedia.org/wiki/NASA_Astronaut_Group_2
today's featured article!

>> No.14854793

>>14854740
Honestly it's a major concern. Who knows how a woman's ovaries might react in such close proximity to the moon; that is how they get their periods after all.

>> No.14854805

>>14854588
Imagine it starship and the booster work flawlessly and imply the concept is sturdy and stable and a twice as big in all dimensions starship and booster work as well

>> No.14854807

>>14854793
Maybe we could inhibit their hormones. could we give them testosterone? is there an aerospace grade? or better yet leave them at home to watch the kids

>> No.14854808

>>14854805
>a twice as big in all dimensions starship and booster work as well
unnecessary with orbital refueling

>> No.14854811

It's that easy in rocketry

>> No.14854818

>>14854784
>back row L to R
no piloting skillz, got rekt
prick
legend
F
Galapagos tortoise
>front row L to R
class clown
manlet
robot
most accomplished astronaut ever

>> No.14854826

so uh...how is starship supposed to stay powered during the lunar night?

>> No.14854836

>>14854826
Methane oxygen generator like zubrin intended

>> No.14854839

>>14854836
speaking of zubrin, when is he going to space? someone crowd fund him a trip on bezos's dildo.

>> No.14854847
File: 40 KB, 152x254, Sickos.png [View same] [iqdb] [saucenao] [google]
14854847

>>14854593
>Personal Hygiene and Body Waste
What was that about Artemis being an all-female program?

>> No.14854849

>>14854826
i don't think there's any plans for that yet. you could stay months at the south pole with continuous illumination.
it only becomes a problem when you're talking about permanent habitation

>> No.14854852

>>14854818
Pete Conrad was so based. Big F to the class clown

>> No.14854861

Here's my organized version of the SLD documents. https://easyupload.io/mxlgob

>> No.14854864

>>14854683
There's no way that Starship is going to be piloted down. That thing is too massive to joystick it during landing. You could fly it in space though. It's basically a SuperMAV from The Martian.

>> No.14854868

>>14854698
360Gbps is such overkill for the Moon in bandwidth that the notional difference between 360Gbps and 1.2Tbps as a result is non-existent. They're effectively the same for Artemis for the ENTIRE decade.

>> No.14854873

>>14854861
good lord anon this is like 9 gigs of krystal porn...i mean it's funny but seems like going really for for a joke

>> No.14854875

engineerlet here, why do jet engines and gas turbines have relatively high exhaust temperature compared to their combustion chamber temperatures, rocket engines as a comparison have a much lower exhaust temperature relative to the combustion chamber temperature

>> No.14854879

>>14854861
Good lord

>> No.14854887

>>14854747
>Midday Meal
>0 hours
The American taxpayer will never stand for this monstrousness.

>> No.14854891

>>14854747
This is because every other HLS lander except for Moonship will not have the operational flexibility to fuck arounxd and have a good time. If the goal of Artemis is to have a maximum of 4 people on the Moon at any given time, and two of those missions are going to leverage HLS Starship. What the fuck are you going to do in an 8 story tall apartment building where each floor is approximately 9x9x9 feet? There's enough space in HLS Starship that you can LITERALLY assign two whole decks PER crew member as habitation volume. But anything BlOrgin or NatTeam or Boeing solo or LockMart solo or any other company solo or ESA or JAXA brings to the table on average will be 1/8th that AT BEST.

It's going to take upwards of 20 fucking years for anyone not SpaceX to catch up with HLS Starship in 2023. No shit NASA HAS to meticulously document everything and every activity with planning and contingencies upon contingencies upon contingencies. HLS Starship can literally have half an entire deck as a hospital. In fact, I fully expect it to be treated as a one with all other landers and crew on the Moon effectively treating it as a landmark where they go to in case of an emergency. It's not out of the realm of possibility that by Q4 2025-2026, there may be at least 3 HLS Starships on the Moon at any given time and 1 more in orbit or docked to the gateway.

>> No.14854904

>>14854891
You're too optimistic. Expect them to go down on the number of refueling launches to 'mitigate risk' until Starship has similar payload capability to the lunar surface as the smaller landers.

>> No.14854905

https://youtu.be/DPPQ0ht0XCI
Dolphin Double Penetration

>> No.14854909

>>14854655
But can it stablely land on the moon and take off again

>> No.14854927
File: 190 KB, 1280x1423, Fc30nqIXgAAMkq1.jpg [View same] [iqdb] [saucenao] [google]
14854927

Listen jack, 15g escape system is perfectly safe
Now get in the pod

>> No.14854936

>>14854904
doubt

>>14854909
it should. only 36% gravity to deal with.

>> No.14854940

>>14854909
It's got a massive ring of RCS thrusters on top to keep it from tipping over

>> No.14854942

>>14854927
Whether or not New Origin killed astronauts, IT DOESNT MATTER. NTSB and FAA must press charges as if they did, and be prosecuted to the maximum extent. This can never happen again

>> No.14854945

>>14854875
Different fuels, cold rocket fuel, different methods of combustion, (maybe different pumping systems?) I would geuss but I hope someone who actually knows answers

>> No.14854947

If pure co2 is available what's the best way to separate the oxygen and carbon

>> No.14854950
File: 37 KB, 783x436, lol.png [View same] [iqdb] [saucenao] [google]
14854950

>> No.14854951

Extraterrestrials were found, disovered by the US coastguard. Documents are highly classifified, unlikely that i can retrieve them,but at least I can attest to their existence.

>> No.14854952
File: 160 KB, 791x557, mm sev space.jpg [View same] [iqdb] [saucenao] [google]
14854952

>>14854425
MMSEV bros is it happening?

>> No.14854956

>>14854952
Sit yo Notional Cargo ass down

>> No.14854970

>>14854951
This man is delusional. Take him to the infirmary.

>> No.14854979
File: 39 KB, 846x406, not just NASA.png [View same] [iqdb] [saucenao] [google]
14854979

>>14854950

>> No.14854987
File: 33 KB, 760x450, comments2.png [View same] [iqdb] [saucenao] [google]
14854987

>>14854950
>>14854979
So many parallels its amazing

>> No.14854990

>>14854950
>quoting random nobodies in a discus comment section

construction of the first ship of the Zumwalt class began in 2011 and it entered service in 2020

>> No.14854993

>>14854990
>doesn't get the point
This contract fuckery and disappointing long wait for inferior, less capable systems isn't just unique to NASA, its our military too, especially the Navy

>entered service
Without a functioning main gun system

The Zumwalt or LCS are the SLS of the US Navy

>> No.14855003

>>14854826
Avg American home uses ~30 kwh per day

Tesla Model S has 100kwh battery pack. Thats' 3 days of electricity.

Add in a solar panel that recharges and you're good to go.

>> No.14855005

F35 is the SLS of the Air Force

>> No.14855007

>>14855005
It is

>> No.14855011

>>14854993
>discus randos give a cool story bro about mil contracts they have no actual knowledge of

The AGS guns of the Zumwalts are fully functional as are their 80 vls cells.

>> No.14855013

apparently other countries are buying the F-35 so I wouldn't say it's exactly SLS...

>> No.14855014

>>14855011
Yeah, the gun works it just costs a million dollars to fire IIRC

>> No.14855015

>>14855011
>>discus
From https://news.usni.org

>the AGS guns
Have no ammo and the Navy is stripping them to replace with hypersonics, do try and keep up https://news.usni.org/2022/03/16/latest-zumwalt-hypersonic-missile-installation-plan-calls-for-removing-gun-mounts

>> No.14855019

>>14855005
The SLS is the best performing and cheapest heavy lift rocket?

>> No.14855021

>>14855019
lol don't even start, F-22 shits all over the F-35 in A2A

F-35 tries to be a jack of all trades

>> No.14855027
File: 143 KB, 1280x1005, FlamyEndDown.jpg [View same] [iqdb] [saucenao] [google]
14855027

>>14855019
f-35 is an abomination. Just look at the damn thing. How much money did they spend on the vertical landing capability. In 2022 any plane could be made to land vertically by just adding landing legs to the rear and landing it like F9, obviously this would require control software but that is much simpler than this convoluted nozzle

>> No.14855030

>They're turning the Zumwalt into an arsenal ship

Should've just done that from the start

>> No.14855034

>>14855015
USNI uses disqus for its comments

>hypersonics

Yes the Zumwalts are getting APM cells in place of the rear AGS mount, a comment like "Without a functioning main gun system" still makes you look like a moron.

>> No.14855038

>>14855034
Can't function without ammo

>> No.14855043
File: 863 KB, 280x280, BasedNozzle.gif [View same] [iqdb] [saucenao] [google]
14855043

>> No.14855046

>>14855043
Canadarm joint but with a jet engine at the end

>> No.14855047
File: 1.40 MB, 4096x2925, FP_1ymoakAMwP3N.jpg [View same] [iqdb] [saucenao] [google]
14855047

>>14855021
You would rather be in an F-35 than an F-22, that an F-22 shits over everything else is just a reminder of how fucking scary it would be to have to face an F-35. And that isn't even taking into consideration that production lot 15 will bring the total number of F-35 to over 900 aircraft.

>> No.14855049

>>14855047
900 too many, could have bought like 10 SLS's with that money

>> No.14855051

>>14855047
They went with the f-117 strategy to make tat sensor in the front stealthy. I think that's an IR cam

>> No.14855055
File: 132 KB, 735x864, usborne books world of the future space mining.jpg [View same] [iqdb] [saucenao] [google]
14855055

>> No.14855064
File: 899 KB, 1600x1067, 1418268390600.jpg [View same] [iqdb] [saucenao] [google]
14855064

>>14855051
Yes that 'glass' box under the nose is a powerful IR sensor.

>> No.14855065

>>14855027
Tail sitters were explored even before thurst vectoring, it's not new. The problem it would have is exactly what Harriers suffered from. While landing the exhaust quickly gets drawn into the intake and the engine heats up. This is why the F35 has a lift fan.

>> No.14855069

>>14855005
nah
F-35 is actually fairly cost effective now when the development cost spreads out over many orders from all over the world
they are under $80M a piece - less than Rafale, Typhoon, Su-35, J-20, etc.

>> No.14855078
File: 151 KB, 1920x1080, mechazilla florida.jpg [View same] [iqdb] [saucenao] [google]
14855078

>> No.14855081

>>14855005
End this meme.

>> No.14855085
File: 193 KB, 1200x630, Beastie Boys, Voskhod 1.jpg [View same] [iqdb] [saucenao] [google]
14855085

Before their music career, the Beastie Boys had a brief stint as cosmonauts. In 1964, the future hip hop trio flew to space aboard Voskhod 1. Although he died tragically in the Soyuz 1 disaster, Adrock reportedly said "fuck that bullshit!", came back to life, and formed the group with the others. The experience later prompted them to write "Intergalactic".

L-R: Adrock, Mike D, MCA

>> No.14855091

>starlink launch scrubbed again

>> No.14855095

>>14855047
Was it purposefully made to look like an eagle?

>> No.14855100

nothings happening in SPAACEFLIIIGHT

>> No.14855113

>>14855091
https://www.youtube.com/watch?v=j_ekugPKqFw

>> No.14855123

>>14854951
Do what we do with all aliens the coasties find: tow them back to Havana.

>> No.14855142

If you structured starship with same materials but more like an N1, basically tapering with a large flared base would you get a benefit out of it? Maybe not as aggressive as an N1 but tapering till a thinner starship version

>> No.14855144

>>14855142
They only did that because they needed extra diameter to fit the engines they needed

No such need exists for superheavy

>> No.14855145

>>14855100
we need more people in SPACE

>> No.14855148

https://www.planetary.org/articles/tianwen-3-china-mars-sample-return-mission
China might grab the Mars sample achievement first.
What else the Chinese might try to do first before everyone else?

>> No.14855155
File: 72 KB, 1249x602, lock mart cev shaps moon.jpg [View same] [iqdb] [saucenao] [google]
14855155

>>14854367
Shapsule

>> No.14855177
File: 118 KB, 947x856, Robert Watts Lunar Roving Vehicle m.jpg [View same] [iqdb] [saucenao] [google]
14855177

>> No.14855179

>>14855145
That starts by having more people on EARTH.

Why aren't you out there having sex, /sfg/?

>> No.14855183

>>14854508
Gonna put a Tesla on the Moon, of course.

>> No.14855192

>>14855148
>First Polar moon landing
>First far side moon landing
>First woman on moon

>> No.14855193

>>14855144
what about aerodynamics gains? yay or nay?

>> No.14855209
File: 251 KB, 1479x946, Diagram_of_steam_locomotive_components_(March_2021_version).tif.jpg [View same] [iqdb] [saucenao] [google]
14855209

Why are we so late, anons?

>> No.14855217
File: 397 KB, 640x512, 1663457973908963.png [View same] [iqdb] [saucenao] [google]
14855217

>>14855021
The F-22 is much more comparable to SLS.
It was cancelled after only a handful built because it cost far too much and there was no reason for it to exist.

The F-35 would probably also beat an F-22 in air to air combat as well, the F-22 is not well equipped to deal with stealth aircraft, lacking EOTS/IRST.
Also it's big supercruise advantage over the F-35 would only increase it's thermal signature and make It easier to detect.

>> No.14855218
File: 660 KB, 1920x1280, Cutaway_steam_locomotive.jpg [View same] [iqdb] [saucenao] [google]
14855218

Imagine a steampunk zinc plated swirling ion bath.
>In Ancient India,[when?] saltpeter manufacturers formed the Nuniya caste.[15] Saltpeter finds mention in Kautilya's Arthashastra (compiled 300BC - 300AD), which mentions using its poisonous smoke as a weapon of war,[16] although its use for propulsion did not appear until medieval times.
>In 1785 Henry Cavendish determined its precise composition and showed that (nitric acid) could be synthesized by passing a stream of electric sparks through moist air.[32]

>> No.14855219
File: 10 KB, 500x220, Nitromethane_anion_resonance.jpg [View same] [iqdb] [saucenao] [google]
14855219

What about a polyether of it?

>> No.14855221
File: 859 KB, 1413x1716, 1972 - Apollo 17 series stamp 3 - (1 Riyal).jpg [View same] [iqdb] [saucenao] [google]
14855221

>>14853340
19 stamps from the Sharjah state of the UAE, 1964-1972

https://drive.google.com/drive/folders/13ImXjO2dgN3uQNkjKMqmmsyntCKrrJsV?usp=sharing

>> No.14855224
File: 555 KB, 1382x2048, EvwQLdzU8AEZjLs.jpg_large.jpg [View same] [iqdb] [saucenao] [google]
14855224

>>14855193
Aero is really marginal for rockets, especially bigger rockets.
The main reason the N1 was designed the way it was, was because it use spherical, explosively formed fuel tanks, since the USSR could not produce large cylindrical pressure vessels.

>> No.14855225
File: 930 KB, 1668x1668, 1964 - Satellite series stamp 1 - OAO-1 - (1 NP.).jpg [View same] [iqdb] [saucenao] [google]
14855225

>>14855221
Not sure about this one, AOA-1 stamp apparently made 2 years before it was actually launched

>> No.14855229
File: 946 KB, 1736x1444, 1972 - Planetary exploration series stamp 5 - Von Braun lunar cabin - (1 Riyal).jpg [View same] [iqdb] [saucenao] [google]
14855229

>>14855225
And a smaller series on von Braun's stations and spacecraft

>> No.14855232

>>14855148
Assuming they actually pull it off

They've yet to encounter the Mars curse

>> No.14855236

>>14855192
>First Polar moon landing
>First far side moon landing
Those could beat Artemis only if delays even more, which is a possibility
>First woman on moon
This is just political shlock, same as "first non american on the moon" or whatever.
I'm talking about actual technical feats. I guess an asteroid landing (possibly an Earth trojan) could be something feasible for China.

>> No.14855246
File: 1.64 MB, 1260x720, Skylab.webm [View same] [iqdb] [saucenao] [google]
14855246

>>14855229
This one looks cool. Reminds me of Skylab.

>> No.14855255

>>14855246
Space ballet is for real man

>> No.14855265

>>14855236
Artemis 3 would need to be delayed by 5+ years just to give China a chance under their most optimistic timeline.

>> No.14855276
File: 11 KB, 594x110, yeahright.png [View same] [iqdb] [saucenao] [google]
14855276

>> No.14855293
File: 87 KB, 1600x900, cover10.jpg [View same] [iqdb] [saucenao] [google]
14855293

>>14855276
>no trolling allowed
It's over musk bros...

>> No.14855311

>>14855276
https://spacenews.com/u-s-weighing-options-to-compensate-commercial-companies-if-satellites-are-attacked/

>If private sector satellites become part of a hybrid public-private space architecture, “then we have some obligation to think about commercial protection,” David Gauthier, director of the National Geospatial Intelligence Agency’s Commercial and Business Operations Group, said at the Intelligence and National Security Summit hosted by AFCEA International, and the Intelligence and National Security Alliance.

>> No.14855329

>>14855276
Reminder
https://spacenews.com/spacex-president-gwynne-shotwell-we-would-launch-a-weapon-to-defend-the-u-s/
>SpaceX President Gwynne Shotwell: ‘We would launch a weapon to defend the U.S.’

>> No.14855338

>>14855329
>The room packed with Air Force service members and military contractors burst into applause. They seemed impressed that SpaceX is one of the world’s coolest companies and also a staunch patriot.
Who wrote this shit? kek

>> No.14855384

>>14855338
The entire apparatus that makes the MIC churn is the image of looking cool and getting paid to do.

>> No.14855398
File: 2.25 MB, 1x1, HLS-PAP-018_HLS White Paper Initial Evaluation of Non-Polar Access Implications for the Human Lander System _Rev_C.pdf [View same] [iqdb] [saucenao] [google]
14855398

this is interesting

>> No.14855404
File: 367 KB, 1x1, JS-2013-002_History_of_Manual_Crew_Override_Rev_A_030713.pdf [View same] [iqdb] [saucenao] [google]
14855404

>> No.14855406
File: 1.93 MB, 1x1, HLS-PAP-008 LETS White Paper Lunar Landing Site Characterization_v3.pdf [View same] [iqdb] [saucenao] [google]
14855406

>> No.14855408
File: 385 KB, 1x1, HLS-PAP-026_Considerations for Fire in Lunar Gravity_Baseline.pdf [View same] [iqdb] [saucenao] [google]
14855408

>> No.14855411
File: 1.37 MB, 1x1, HLS-PAP-025 HLS Active TRN Whitepaper_Rev_A.pdf [View same] [iqdb] [saucenao] [google]
14855411

>> No.14855413
File: 758 KB, 1x1, HLS-PAP-012 HLS White Paper HLS Navigation Beacon.pdf [View same] [iqdb] [saucenao] [google]
14855413

>> No.14855419

>>14855404
NASA's still the only agency that requires the manual crew override

>> No.14855437

Test

>> No.14855454

https://www.youtube.com/watch?v=SuEmD9WRKes
yeah

>> No.14855456

>>14855276
Yet another Muskian lie

>> No.14855471

>>14855329
that whole article is full of based Shotwell quotes
>"I was hoping to beat the Chinese this year,” she said. “It does concern me that China is flying 40 times this year. And it’s not for commercial customers. They have very few commercial customers. So what in the world are they doing?” she added. “The fact that I’m not beating them is a shame. The fact that they’re launching 40 times is something we should all be worried about.”
This was back in 2018. it looks like SpaceX is on track to beat China in launches for the first time this year

>> No.14855508

>>14854875
Much greater expansion ratio. Expand gas more, it cools off more. Simple as.

>> No.14855509

>>14854909
Yes easily

>> No.14855511

>>14855471
While China's raw numbers are impressive at first glance, at least 80% of their launches are on first generation Long March rockets. The LM-3B/E is a near peer to the Falcon 9 but it's only a fraction of those launches. In terms of mass to orbit its not even a contest.

>> No.14855515

>>14855511
Dont say that out loud, we need to scare Congress

>> No.14855518

>>14855142
N1's structural design is worse than a straight cylinder in every aspect. Yes, every aspect, including that one you just thought of.

>> No.14855522

>>14855518
but it looks cool

>> No.14855525

>>14855329
Based mommy Shotwell, I must worship her body

>> No.14855529

>>14855525
i'm still waiting for her swimsuit pics

>> No.14855538

>>14855522
you can't prove that

>> No.14855540

>>14855529
I should learn how to use stable diffusion or one of those other AI image generators

>> No.14855565
File: 364 KB, 646x595, sweaty2.png [View same] [iqdb] [saucenao] [google]
14855565

>>14855091
>>14855113
Did the ruskies upgrade their HAARP clone, bros?

>> No.14855598

>>14855565
The atmosphere is merely rebelling, upstart that it is.

>> No.14855635

Holy fuck I didn't know that general public looking at computer screens can help discover exoplanets 1000s of light years away
https://www.zooniverse.org/projects/nora-dot-eisner/planet-hunters-tess/talk

>> No.14855744

lmao why do astronomy papers have like 20 coauthors

>> No.14855747

>>14855744
Depending on where you work, publishing output is a tracked metric

Also if your work uses someone else's software or instrument it's typically seen as a courtesy to add them as co-authors since they contributed -- look at some of the New Horizons papers for instance

>> No.14855889

>Alpha is also intended to be a direct American competitor in the small satellite market to India's Polar Satellite Launch Vehicle (PSLV), as the company believes that PLSV's ride-share capability threatens U.S. domestic launchers in this market.[17]
Bloddy benchode bastard may your cows go barren

>> No.14855891
File: 68 KB, 1024x766, 1635518723237.jpg [View same] [iqdb] [saucenao] [google]
14855891

>>14855246
>Born too late to be a Skylab astronaut
>Born too stupid to be a starship pilot

Why should I even live?

>> No.14855897

>>14855891
Born just in time to give Elon Musk 1billion dollars to take you on a moon cruise

>> No.14855899

>>14855891
They might let you fly junker starships after they're EOL

>> No.14855902

>>14855889
Skyroot aerospace and sslv will destroy the american small sat market

>> No.14855952

> TESS was expected to ultimately detect about 1,250 transiting exoplanets orbiting the targeted stars, and an additional 13,000 transiting planets orbiting additional stars in the fields that TESS would observe.[12] As of 5 April 2021, TESS had identified 2,601 candidate exoplanets, of which only 122 had been confirmed
uh-oh

>> No.14855974

>On 25 January 2021, a team led by astrochemist Tansu Daylan using the Transiting Exoplanet Survey Satellite (TESS), with the help of two interns, Jasmine Wright (18) and Kartik Pinglé (16) as part of the Science Research Mentoring Program at Harvard & MIT, discovered and validated four extrasolar planets — composing of one super-earth and three sub-neptunes - hosted by the bright, nearby, Sun-like star HD 108236. The two high schoolers, 18 year old Jasmine Wright of Bedford High School in Bedford, Massachusetts, and 16 year old Kartik Pinglé of Cambridge Ringe And Latin School, of Cambridge, Massachusetts, are reported to be the youngest individuals in history to discover a planet, let alone four.[80][81]
When I was 16 I was busy reading 4 fucking chan

>> No.14855982

>>14854197
hey, stop being ungrateful. that's an increase in survival rate compared to no abort system at all!

>> No.14856047
File: 209 KB, 668x729, FTpezL2XsAE1x0g.png [View same] [iqdb] [saucenao] [google]
14856047

IT HAS BEEN TWO YEARS AND NOTHING BIG HAS LEFT THE GROUND

It is all craneing and VABing around unflyable cilinders.

You guys told me we were entering a new era of spaceflight...

Until when am I supposed to wait?

>> No.14856062

>>14856047
https://www.youtube.com/watch?v=rdpBZ5_b48g

When September ends

>> No.14856264

>>14854568
>You’ll be hearing from my lawyer about the 1g you owe me!

>> No.14856292

>>14854197
imagine if they had killed william shatner with a 15g abort

>> No.14856310

>>14856062
and here I was thinking I only had to wait until the 21st... https://www.youtube.com/watch?v=Gs069dndIYk

>> No.14856312
File: 41 KB, 640x465, Soyuz_T-10-1_abort.jpg [View same] [iqdb] [saucenao] [google]
14856312

>>14854197
Nothingburger
>the escape system motor fired, dragging the orbital module and descent module, encased within the upper shroud, free of the booster with an acceleration of 14 to 17g (137 to 167 m/s2) for five seconds.
>The two crew members were badly bruised after the high acceleration, but were otherwise in good health and did not require any medical attention.
>Upon being greeted by recovery crews, they immediately asked for cigarettes to steady their nerves. The cosmonauts were then given shots of vodka to help them relax.

>> No.14856338
File: 1.71 MB, 1884x2739, 1632182016724.jpg [View same] [iqdb] [saucenao] [google]
14856338

>>14855522
Sure, but not coolER.

>> No.14856367

https://twitter.com/thesheetztweetz/status/1571484240319053825
>Asked when a permanent base will be established on the moon, NASA’s @SenBillNelson says “it may not be permanent in the sense of 365 days a year, but you could certainly be there for extended periods of time in order to learn how to exist in a very hostile environment.”
moon base bros...

>> No.14856378

>>14856367
A permanent moon base should not mean the base itself is permanently placed there but mostly unused.

>> No.14856382

>>14856367
Who cares about NASA moon base? It'll be private.

>> No.14856383

>>14854987
Not surprising.

>> No.14856406

>>14856367
Considering the fact that the first permanent habitat isn’t slated to be sent until Artemis VIII in 2031 (read 2038 assuming it hasn’t been cancelled yet) I’m gonna go out on a limb and say the answer is “never”

>> No.14856411

>>14856406
my source is NASA’s own moon to mars manifest in case you don’t believe me

>> No.14856417

>>14856406
the first permanent habitat will be private, mark my words. spacex has expressed interest multiple times in creating a large moon base and i imagine they'll collaborate with some private institutions to do this

>> No.14856418

>>14856367
Ballast Bill is a fucking coward and an elderly fuck. NASA needs to be led by somebody with still functioning testes.

>> No.14856496
File: 710 KB, 1920x1080, raptor_blast_shield.jpg [View same] [iqdb] [saucenao] [google]
14856496

Neat, they're testing blast shields for raptor with destructive tests, very nice green color.
https://twitter.com/thejackbeyer/status/1571424035291901952

I wonder what's the most reliable way to blow up a raptor

>> No.14856502

>>14856496
>we're trying to remove the shrouds, best part is no part
>if the raptors are fireproof we delete the shrouds
>...
>we're adding blast shields
What did he mean by this?

>> No.14856515

>>14854592
yeah when i tried to give some lucky bums and prostitutes free rides on my suborbital rocket's abort test they hit me with a kidnapping charge

>> No.14856524
File: 764 KB, 1200x1206, Screen Shot 2022-09-18 at 10.45.12 AM.png [View same] [iqdb] [saucenao] [google]
14856524

>> No.14856540

>>14856524
are those liquid boosters?

>> No.14856541

>>14856524
So, by 2035 they'll have started reusing the cheapest and most easily expendable part of the rocket?

>> No.14856547

>>14856524
So it's like an itty bitty Starship you launch with a normal expendable rocket, it deploys the payload then deorbits for next use? Could be neat, but the main stage should be reusable too. Why throw any of the rocket away if you can help it?

>> No.14856559

>>14856524
wont the payload hit make the rocket less economical than flying expendable?

>> No.14856593

>>14855952
I don't know what they were thinking giving TESS so short an observation time for most of the sky

>> No.14856596

>>14856047
>IT HAS BEEN TWO YEARS
It will have been two years by May 2023, calm down space is hard etc

>> No.14856600

>>14856367
Private moon base funded by Jared Isaacman will be set up at the north pole and will put immediate focus on installing MOE units to generate aluminum and iron metal feedstock in-situ. They will do effectively zero scientific research apart from mineral prospecting and slope stability studies around them, and that's a good thing (nerds seething)

>> No.14856603

>>14856502
>we're trying
He means they're trying but the Booster is coming along faster than the lack of need for blast protection, so they're adding blast protection in the mean time which they may get rid of later.
>>14856496
Imagine having so many engines that using them as consumables during engine blast shroud development makes sense, lolol

>> No.14856605
File: 264 KB, 2048x1536, Fc8bZ2cWAAUmUTV.jpg [View same] [iqdb] [saucenao] [google]
14856605

>>14856524
Not even a reusable second stage. I'm not sure what the hell this is supposed to be. A vertical landing shuttle?
There's also a picture of this on top of a Falcon 9 clone.

>> No.14856606

>>14856540
They appear to be the exact same Ariane 6 solid boosters. This makes sense given that they said this thing only replaces the upper stage of the launch vehicle.

>> No.14856608

>>14856605
>There's also a picture of this on top of a Falcon 9 clone.
post it

>> No.14856611
File: 236 KB, 1536x2048, Fc8bZ2iXoAAe165.jpg [View same] [iqdb] [saucenao] [google]
14856611

>>14856605
>>14856608

>> No.14856616
File: 296 KB, 2048x1536, Fc8bZ2fWAAEzovj.jpg [View same] [iqdb] [saucenao] [google]
14856616

>>14856611
starship animation vibes

>> No.14856619

>>14856611
Weird that this is basically just a reusable space capsule, but it's being rebranded as a reusable upper stage. If it were a reusable upper stage they wouldn't need that middle expendable stage in there.

>> No.14856620
File: 253 KB, 2048x1536, Fc8bZ2iWAAEE7vI.jpg [View same] [iqdb] [saucenao] [google]
14856620

>>14856616

>> No.14856624

>>14856616
oh please, this is so gay

>> No.14856626
File: 172 KB, 2048x1536, Fc8XJ1dWYAE2gMC.jpg [View same] [iqdb] [saucenao] [google]
14856626

>>14856620
last pic I got

>> No.14856627

>French engineering
They say 2035, so we can expect delivery 2055.

>> No.14856631

>>14856605
Seems to me like a sort of smart payload attachment system. Attach some experiments to it and return to earth.

>> No.14856634

>>14856611
>>14856616
So kinda like the Stoke Aerospace thing except worse because it doesn't reenter bottom first, taking advantage of the conical shape.
>>14856626
those control surfaces are like 5 times too big

>> No.14856637
File: 216 KB, 960x1015, Rockets Violate Conservation of energy.jpg [View same] [iqdb] [saucenao] [google]
14856637

>> No.14856639

fuck off mandlbimbo

>> No.14856642

The euro capsule isn't too bad if it has crew capability, because they could use one, but they should probably just go for a standard capsule (or all-in on a fully reusable system) instead

>> No.14856645

>>14856619
manned?

>> No.14856670

>>14856642
India is soon going to have crew capability.
Yet, Europe, the birth of industrialisation, the conquerors, the empire where the sun never sets, the very same people who bridged east and the west..
doesn't have one?

>> No.14856676

>>14856626
Why is it squared?
And what are those stupid plastic flaps?

This is fucking retarded.

>> No.14856683

>>14856676
>anon doesn't understand microaerodynamics on the spaceflight general

>> No.14856688

>>14856670
too much socialism

>> No.14856701

>>14856637
It seems he is confusing a few things because as-written, it makes no sense.

>> No.14856708
File: 41 KB, 1210x92, Selection_370.png [View same] [iqdb] [saucenao] [google]
14856708

>>14856688
India is socialist tho

>> No.14856707

>>14856631
It's a crew capsule combined with a reusable payload faring, which has the advantages of reducing the payload mass fraction of each launch, limiting payload volume, complicating launch ops since you're tying a crewed vehicle to this thing, and making human launch more clunky by carrying this payload volume around, and it does it all without having any effect on speeding up launch cadence or reducing launch costs.
Truly, euro engineering prowess can be frightening at times

>> No.14856709
File: 1.61 MB, 960x540, astra LV0006 does the BLM shuffle.webm [View same] [iqdb] [saucenao] [google]
14856709

>>14854238
Here's a demonstration of 1g of thrust, by the way.

>> No.14856712

>>14856637
>south africa
hahahahahaha

>> No.14856713

>>14856708
India is a feudal state.

>> No.14856715
File: 124 KB, 400x400, RP-1-Logo-400px.jpg [View same] [iqdb] [saucenao] [google]
14856715

>>14853513
Just did my first Lunar orbits using a Gemini pushed by a duel RL-10 Centaur clone.
Working on a 4-launch landing mission now, I don't have high enough thrust engines to do an Apollo clone so I'm going to launch the lander, a centaur to get it to LLO, another centaur and them the Gemini that it'll send to LLO.
Hoping to get 2 man landing done by '68 this game.

>> No.14856716

>>14854305
That means crew Starship, then. There's no other system even in development that can handle lunar reentry.

>> No.14856717

>>14856670
they fell off

>> No.14856718

>>14856717
They hit the wall.

>> No.14856719

>>14856676
It's one of the worst approaches to partial reusability I've ever seen

>> No.14856723

>>14856717
>>14856718
They had their entire population of confident risk-takers torn up in world war 1 and world war 2 back to back

>> No.14856732

>>14853835
You don't need twitter to watch videos of them all running engine rich around the 8 second mark. The 2 still doesn't hasn't had a full duration burn.

>> No.14856738

>>14856732
Shoo shoo. They are burning the engines hard enough to destroy them on purpose.

>> No.14856741

>>14856738
>don't complete a standard pressue run
>start pushing them beyond design pressure from day one
This makes perfect sense, I will never question the great SpaceX again.

>> No.14856742

https://twitter.com/JeanMarc_Nasr/status/1571477490639454208
/ourfrog/

>> No.14856748

>>14856742
God, I wish

>> No.14856759
File: 652 KB, 3000x2400, 275102main_EC85-33180-1_full_full.jpg [View same] [iqdb] [saucenao] [google]
14856759

Mai Waifu

>> No.14856763

>>14856759
ugly

>> No.14856765

>>14856524
COOL i dont even care if it sucks, at least they're doing something

>> No.14856771
File: 118 KB, 598x483, Hermes1.jpg [View same] [iqdb] [saucenao] [google]
14856771

>>14856765
>at least they're doing something
>she doesn't know

>> No.14856776

>>14856541
Second stages are often much more expensive than first stages despite being smaller because mass is so critical.
You can have a fat first stage and it's not a big deal, have a fat second stage and your first stage just had to get bigger.

>> No.14856779
File: 236 KB, 1536x2048, Mrczd9O.jpg [View same] [iqdb] [saucenao] [google]
14856779

>>14856541
>>14856547
it's agnostic, picrel
>>14856559
yes, reusability is a scam (always has been). proof posted below
https://on.soundcloud.com/QFXou

>> No.14856789

>>14856771
I will never be a woman, but Hermes 2.0 is BACK and it's not a spaceplane so it'll actually work so commence seething. also ESA is requesting a 25% increase in budget soon. Europe will send astronauts to space before India, sir

>> No.14856793

>2006: NASA contractors decide not to pursue FFSC engine development after they built and tested the integrated powerhead demonstrator
>2022: SpaceX is building the Raptor engine at a rate of 1 per day for a price tag of less than $2 million pessimistically. Also Raptor is the highest pressure engine of all time and the highest Isp non-hydrolox chemical engine of all time
Anons, where did it go so right? And what the fuck was Rocketdyne and Aerojet's problem?

>> No.14856794

>>14856779
>Soundcloud now requires an account to skip ahead
I hate the technokikes.

>> No.14856801

>>14856794
hmm I was able to without an account

>> No.14856803

>>14856801
ditto

>> No.14856805

>>14856779
>reusability is a scam
First stage has been proven, by scaling up you make the mass fraction landing costs you negligible. Second stage is yet to be seen, Shittle fucked it up but it also kept reusing solids despite that costing more than junking them thanks to politcs.
When SpaceX was talking about film cooling the second stage I was so happy they had done away with tiles which have proven a huge issues to reusability... We'll see if tiles can be made to work but I have doubts.

>> No.14856806

Instead of developing the Raptor engine, SpaceX could've invested a bit of R&D in Merlin to make it more reliable and powerful and just used it on Starship.

>>14856741
>This makes perfect sense, I will never question the great SpaceX again.
based

>> No.14856809

>>14856806
Though they would need to add an extended base to the booster or just make the entire rocket shorter and wider

>> No.14856812

>>14856793
They thought they could get by forever on an endless stream of RL10 modifications. They also bought into the idea that idea that rocket engines were super hard and they were the only ones who could do it and that no one could do at all it without billions of dollars of money from the government. Since the government would never fund anyone who wasn't them they didn't have to worry about any competition.

>> No.14856816

>>14856524
>>14856605
HERMES IS BACK BABY

>> No.14856820

>>14856806
The Merlin is too inefficient and kerolox pretty shit for reusability. Sounds like an awful idea.

>> No.14856821

>>14856806
>just make the Merlin more reliable
what did he mean by this?

>> No.14856823

>>14856806
They wouldn't need to change Merlin at all, just use more on each stage. A reusable second stage using three MVac engines and one center Merlin engine for landing, with a first stage that had like 30 Merlins on it. Simple as.
The issue is that this would only be useful for LEO launches, realistically, and would still suffer from soot buildup in turbomachinery resulting in longer refurb times between launches. Best to switch to a new, non-sooty fuel like methane.
If you want to do an analysis and figure out the minimum viable fully reusable TSTO rocket, it probably looks like a methalox fueled vehicle with gas generator powered engines and a total LEO payload mass of like 25 tons. SpaceX has lofty goals for Starship so they want that extra performance afforded by FFSC and they also want big mass to orbit, hence the large scale of the vehicle.

>> No.14856825

>>14856805
I was posting sarcastically. That leaked audio from a now-fired ULA VP displays the full delusion of oldspace

>> No.14856829

>>14856806
Merlin 1D is one of the most reliable rocket engines ever.

>> No.14856830

>>14856524
Can someone explain to me why they are making the second stage reusable instead of the boosters or the core? Why not just copy SpaceX?

>> No.14856838

>>14853617
The acting administrator resigned immediately after his decision in order to force Nelson to accept and run with the HLS selection even though he's the father of SLS. NASA got a once in a lifetime opportunity to dictate their own destiny and did. Congress lost their fucking shit because sales guys seethe and get violent when engineers/nerds dictate terms of the engagement. Congress is like 90% sales guys.

It's a stereotype that sales guys get to drink and rail hot bitches while engineers/nerds toil away. NASA is a nerd organization. HLS Starship is revenge of the nerds.

>> No.14856841

>>14856830
ESA/Ariane simply have no plans for first stage reuse anywhere to be found. /sfg/ already looked

>> No.14856842

>>14856830
First of all they aren't making the second stage reusable, the second stage in their concept remains expendable, the only reusable bit is a payload bay volume and a crew capsule on top. It's more bizarre than you think.
Also the reason for why they don't just copy SpaceX is difficult to pin down at best, but I will say that Ariane group has a lot of pride and I don't think it's out of the question that they are still huffing their own copium and don't actually believe that Falcon 9 style reuse is economic, despite all contrary evidence. They very likely find the fact that someone else is doing it WAY better than they are to be a bitter pill to swallow.

>> No.14856845

>>14856841
I'm trans btw

>> No.14856846

>>14856812
The RL-10 is one of the best engines ever made and based on the market demand for high energy upper stages no one needs anything that can't be done with 2 RL-10.
I can't blame them for thinking they could cruise on it for another 60 years.

>>14856825
Ah k, I just saw it was an hour and closed it.

>> No.14856847

>>14856845
I am transplanetary

>> No.14856848

>>14856838
I put my hands together and pray every night thanking the devil for causing the downfall of those prideful sinners in congress and for torturing them forever upon their deaths

>> No.14856849

>>14856841
Why are you lying?

>> No.14856850
File: 29 KB, 1200x1317, Ethanol.svg.png [View same] [iqdb] [saucenao] [google]
14856850

What do /sfg/ think about ethanol + liq oxygen as fuel for small orbital rockets? or as i like to call it: Loxyhnol

>> No.14856852

>>14856849
You have no evidence of me lying

>> No.14856857

>>14856850
mueller says no, too much coking

>> No.14856858

>>14856841
>>14856842
Are you fucking retarded? They have said for years they want Ariane NEXT to have a reusable first stage. They're literally building and testing prototypes right now (Themis) for it and making engines meant to be cheap and reusable (Prometheus). Ffs this presentation literally has a picture of a reusable Falcon 9 clone.

>> No.14856859

>>14856846
>The RL-10 is one of the best engines ever made
Debatable, it's one of the highest Isp chemical engines ever made but it's also extremely expensive for what you get and it has a pitiful thrust output. I would really love to see someone build a 250 kN FFSC hydrolox engine that beats RL-10 in every performance metric with 1/40th the cost. It wouldn't even be that hard desu, since FFSC dodges all of the rotating seal autism that the RS-25 got fuckered by.

>> No.14856862

>>14856806
good luck turning around a kerosene stage in a couple hours
have fun producing RP1 in situ on mars

>> No.14856863

https://youtu.be/VgPipTFODUg
LADIES AND GENTLEMEN
WE GOT HIM

>> No.14856865

spacex: announces projects and does them
china: doesnt announce projects and does them in secrecy
europe: announces projects but doesnt do them

>> No.14856868

>>14856858
Ariane NEXT is real. You've seen all the renders

>> No.14856869

>>14856842
>the second stage in their concept remains expendable, the only reusable bit is a payload bay volume and a crew capsule on top.
So this big new idea of these is fully reusable, propulsively landed, orbit-capable payload fairings?

>> No.14856873
File: 43 KB, 496x500, 1545964095137.jpg [View same] [iqdb] [saucenao] [google]
14856873

>>14856841
https://www.esa.int/Enabling_Support/Space_Transportation/Future_space_transportation/Test_tanks_fuelled_for_ESA_s_Themis_reusable_first_stage

>> No.14856875

>>14856859
RD-0146D comes somewhat close. Cheaper, more efficiant, higher TWR, about the same thrust.

>> No.14856878
File: 902 KB, 1920x1883, Themis_test_tanks_during_cryogenic_filling_and_draining_tests_pillars.jpg [View same] [iqdb] [saucenao] [google]
14856878

>>14856873
Here's your reusable propane tank bro

>> No.14856879

>>14856862
>they picked methane because it can be made i situ
you swallowed the corporate propaganda

>> No.14856881

>>14856850
>more than one carbon atom in your fuel molecule
NGMI

>> No.14856883
File: 39 KB, 713x461, 1661892647934840.jpg [View same] [iqdb] [saucenao] [google]
14856883

>the /pol/tranny mutt is here
*yawn*

>> No.14856884

>>14856878
we are mere months away from a reusable Ariane booster

>> No.14856886

>>14856858
If Ariane group were rational they would take an axe to all Ariane 6 hardware immediately and literally, and fire 85% of their management staff at the same time.

>> No.14856887

>>14856862
Fuel to return will never be made on mars. What an insane waste of the colony's resources that would be

>> No.14856893

>>14856886
Seeing as Amazon has already bought like 30 launches and probably more in the future that would be fucking retarded

>> No.14856894
File: 20 KB, 620x612, KtaY53DjsohZxxHLajgTUB-1200-80.jpg [View same] [iqdb] [saucenao] [google]
14856894

Could two Falcons land on the same boat?

>> No.14856895

>>14856865
>china: doesnt announce projects and crashes them into villages in secrecy

>> No.14856898

>>14856865
russia: doesn't announce projects and fails them in secrecy

>> No.14856899
File: 153 KB, 1080x1080, pesquet_hug.jpg [View same] [iqdb] [saucenao] [google]
14856899

>>14856884
you're delusional but i respect your conviction

>> No.14856900

>>14856881
>>14856857
Elaborate please, it seems like a decent/cheap choice at first.

>> No.14856901

>>14856869
Pretty much, but the fairings are also manned.
>>14856875
Still an expander cycle though, gimme my travel thermos sized fuel rich and oxygen rich preburner-turbopump assemblies please

>> No.14856903
File: 237 KB, 363x343, lynched.png [View same] [iqdb] [saucenao] [google]
14856903

>>14856900

>> No.14856904

>>14856899
though less delusional than Muskrats that think a starship will be heading Mars in the next few years

>> No.14856905

>>14856899
Looks like the suit is going to pull an sneaky assgrab there

>> No.14856906

>>14856884
A number of months could be literally any amount of time

>> No.14856910
File: 59 KB, 706x671, cheers.jpg [View same] [iqdb] [saucenao] [google]
14856910

>>14856904
hey, i'll drink to that

>> No.14856914
File: 69 KB, 650x1000, cheers56.jpg [View same] [iqdb] [saucenao] [google]
14856914

>>14856910
cheers bud

>> No.14856915

>>14856901
Doesn't expander cycles make the engine weigh less than an FFSC?

>> No.14856917

>>14856884
The Thémis hop is NET 2023, and there's a bunch of other tests after that

>> No.14856921

>The Themis programme will provide valuable information on the economic value of reusability for Europe and prove technologies for potential use on future European launch vehicles.

>> No.14856923

>>14856887
>don't make propellants
>only a very small number of people are willing to go to Mars given that it's saying goodbye to Earth forever, but you have more megajoules to idk make aluminum with or something
vs
>make propellant on Mars
>now you can go live on Mars for two years and come back if you don't like it, many many more people go in total and the number of people who become lifers also increases massively because they realize Mars is fine actually, but you also need to ship in more solar panels in total before Mars solar panel production can catch up to demand
hmm I wonder which one of these scenarios leads to a faster growing Mars colony

>> No.14856924
File: 77 KB, 1122x559, Columbus, the MTFF, Hermes.jpg [View same] [iqdb] [saucenao] [google]
14856924

>>14856816
>>14856771

>> No.14856925

>>14856917
*****NET date does not include covid delays
;)

>> No.14856927

>>14856893
That only makes aborting the A6 rocket funnier

>> No.14856930
File: 83 KB, 720x405, Themis_demonstrations.jpg [View same] [iqdb] [saucenao] [google]
14856930

>> No.14856931

>>14856917
The Themis is like 2/3 of the size of Falcon 9's first stage, why didn't they build a small reusable rocket out of it as their Soyuz replacement?

>> No.14856935

>>14856900
>Elaborate please
Coking (solid carbon deposition) inside fuel rich parts of the engine increases dramatically with increasing number of carbon-carbon bonds inside each fuel molecule, to the point that only lone-carbon-atom fuels are free of coking (for example, methane, methanol, monomethyl hydrazine, unsymmetric dimethylhydrazine). If it's got two carbon atoms bonded to each other, you get coking.

>> No.14856936

>>14856914
hgh gut
i get it but damn dude that stuff isn't magic elon needs to start exercising and slim down

>> No.14856943

>>14856931
They might be only building it to show they meet the green agenda so Europe will give them tax credits

>> No.14856948

>>14856915
No, it just makes it a small engine. RL-10 only has a TWR of like 37.3, but it's simultaneously tiny at 301 kg. A staged combustion engine producing the same thrust output would weigh easily half as much, or for the same mass could produce easily double the thrust, and at higher Isp as well.

>> No.14856949

>>14856901
>the fairings are also manned
Does their innovation have no limits?

>>14856915
A bit lighter and a lot simpler since you don't have to worry about including a preburner or the associated plumping.

>> No.14856952

>>14856859
While it is expensive I don't get the "more thrust" argument, what commercial / military payloads can't wait for a 2 orbit burn?
It can relight hot and cold with no real time limit between ignitions allowing for all the insertion / correction burns you could want.
Despite the cost I would love to see a LUNEX style lander running the RL-10.

>> No.14856953

>>14856930
Looking forward to those hop tests, they must be what, a few weeks away at most?

>> No.14856958

>>14856936
There's not much gut there though, that looks more like rib cage. Not defending the look.

>> No.14856965

>>14856935
Thanks, following that logic, natural gas would be a decent choice then, here is really cheap and only contains one carbon atom as well. so why is kerosene more popular? Is it cheaper on the usa?

>> No.14856974

>>14856948
Depending on the role of the upper stage TWR doesn't mean shit. For SLS the efficiancy and the overall mass of the engine will matter by far the most since the core stage will bring it up pretty much all the way to orbit.

>> No.14856984

>>14856965
Kerosene has higher density and is much easier to handle since it's liquid at room temperature. For none reusable rockets kerosene will always be the better choice because of it.

>> No.14856985

>>14856949
>A bit lighter and a lot simpler since you don't have to worry about including a preburner or the associated plumping.
see >>14856948
Expander cycle is not better than staged combustion, it's only really good looking if you can't do staged combustion yet (like the americans in the 50's and 60's couldn't). Where expander cycle really shines is actually for long lifetime reused Moon lander vehicles, since the expander cycle is a low operational stress power head with an inherently great throttle range and good Isp, and the Moon has low enough gravity and low enough delta V requirements that a super great TWR or mass fraction isn't necessary.
The Soviets built the S1.5400 staged combustion engine in 1960, which had about half the thrust of the RL-10 and a better TWR, so there's no actual issue with going to that small scale. With modern designs and materials a staged combustion hydrolox engine of 100 kN scale would easily beat the mass of the RL-10.
>>14856952
>While it is expensive I don't get the "more thrust" argument, what commercial / military payloads can't wait for a 2 orbit burn?
It's more about the use as a second stage, ie for achieving orbit. You can't split your burn in half if you don't have a periapsis above the atmosphere yet. Also, a higher TWR power cycle means you can build a physically smaller and lighter engine that outputs the same thrust and therefore gives you a lighter stage and better overall performance, even before factoring in the higher Isp that a staged combustion engine affords.
Also yeah, I agree that the expander cycle engine is a good fit for lander craft, what I'm saying is that it's not actually a good fit for launch vehicles, as small staged combustion engines would be superior. The only reason we use the RL-10 for this is because the USA needed a higher Isp engine and they didn't believe staged combustion would be worth pursuing (due to their materials limitations at the time).

>> No.14856988

>>14856887
>>14856923
2 way highway 1000 star ships in total (give or take) 500 at any given time heading to earth, 500 headed to mars, a number remaining on the surface of Mars and maybe in orbit, these numbers can be scaled down and ramped up to if need be

>> No.14856993

Starship should have 150 expander cycle methane engines.

>> No.14856995

>>14856965
RP-1 is just highly refined jet fuel which is just extra refined gasoline. It's not an ideal fuel but it's cheap as fuck and you'll never have trouble finding a supplier.

>> No.14856997

>>14856965
Kerosene is/was more popular because rocket engines were developed after powered aircraft and they piggybacked off of the industrial fuel supply that those aircraft used. It was simply a lot more convenient to tweak jet fuel to be suitable for rocket fuel than it was to invent large scale natural gas extraction and storage and liquification. In modern days though many rocket companies young and old are shifting towards methane as a fuel, because the infrastructure has caught up and the lack of complications from burning long chain hydrocarbons means better engine cycles are available (plus the clean burn allows for easier reuse optimization).

>> No.14857003

>>14856974
It does matter though, I'm not talking about stage TWR I'm talking about engine TWR. If your engine produces the same thrust at twice the TWR, it means your engine weighs half as much, which means your dry mass fraction is reduced, which means your payload mass has gone up and/or your available delta V has increased. You're right that stage TWR doesn't matter much once you're already in orbit, but engine TWR absolutely does always matter. It's why it's tricky to design a NERVA-propelled vehicle that can out perform a chemical rocket; the got dayum engine just weighs so damn much that it eats a lot of performance.

>> No.14857004

>>14856995
>jet fuel which is just extra refined gasoline
isn't jet fuel refined diesel?

>> No.14857008

>>14856923
I'd agree with you but a Mars colonist with a ticket back is called an Earther. For the sake of independence, ISRU propellant plants and outbound Starships must be sabotaged.

>> No.14857011

>>14856985
>achieving orbit
I totally agree, I was thinking about it as a high energy upper for GTO, LTO. MTO ect. All the smart mission designs only have it do a couple of hundred m/s to get orbit and let the second stage reenter.
If we are talking about a second stage engine I agree you need more thurst, I'm sad we are about to see RS-25s used as first stage engines when they would be perfect second stages (using what's left, not building new).

IMO if I was building an expendable second stage these days I would be looking at the tank manufacture costs before deciding a fuel, hydrolox has great ISP but needs big tanks with big dry masses or extremely expensive manufacture.
I might end up running kero or metho just to enjoy more compact packaging and maybe stick it in the fairing to get as much mass as possible off the second stage.

>> No.14857013

>>14857008
>ISRU propellant plants and outbound Starships must be sabotaged
Radically treasonous, Mars will colonize the rest of the solar system while Earth languishes in endless conflict below. The universe belongs to Mars.

>> No.14857014

>>14856995
>RP-1 is just highly refined jet fuel which is just extra refined gasoline
It's less refined, they use it specifically because jet engines will run on anything and kero is cheaper.

>> No.14857022

>>14856965
The reason why Kerosene is popular in rocket is because its a more readily available fuel. For consumer market, thats gasoline. "readily available" means highest energy density at room temperature, which means less hardware requirement to chill, maintain, etc.

The reason why people use kerosene is because cryogenics research had to be done to take advantage of cryogenic fuel procedures. Back when rockets were first being made, the most readily available fuel was ethanol/gasoline/kerosene, etc Physics dictate hydrogen might be good, but required extreme cryogenics. What physics dictates and what engineers work with are two different things. Hydrogen's ups are physics efficiency, but downsides are engineering/operational difficulties.

>> No.14857025

Isn't fuel a fraction of the rocket's cost?

>> No.14857036

The King hath spoken, heed his words ye men of science

https://twitter.com/elonmusk/status/1571540353978859526

>> No.14857037

>>14857003
Miniaturization of engines are not liner, and for staged combustion engines making them smaller often makes them more troublesome to build if you want to keep the same benefits it offers. Expander cycles can be made smaller and smaller while losing less of the benefits they offer. So I'm not too sure simply making smaller hydrolox engines like RL-10 FFSC will actually make them better engines.

>> No.14857041

>>14857036
>Sciencebros will get rideshare discounted costs to orbit

I mean that's great, as long as you're not going interplanetary

>> No.14857049

>>14856995
Jet fuel is kerosene, not gasoline. You seem to have confused it with av-gas, which is not only gasoline, but still leaded.

>> No.14857053

>>14857025
Fuel price means basically nothing in the big picture, what does matter is all the support equipment. Having normal fuel tanks you would find on a farm full of RP-1 is orders of magnitude cheaper than keeping H2 cold and not leaking.

>> No.14857054

>>14857041
>interplanetary
Anything beyond LEO, really, I doubt they'd allow tugs on such missions.

>> No.14857055

>>14857011
RS-25s are not air lightable. At this point a methalox engine with >=380s Isp beats hydrolox every time just for simpler tanking and better overall delta-V. LH2 doesn't become useful again until you get into NTP or laser thermal where the Isp penalty for switching to denser fuel is like 40%.

>> No.14857062

>>14857054
Still high enough to send up a camera and prove that the Earth is flat.

>> No.14857066

>>14857062
>implying big space will let you get a camera onboard without sneaking a fisheye lens on it to make it look round

>> No.14857072

>>14857062
>>14857066
Any camera on a spacecraft that takes a picture of earth has to be specifically cleared by a regulatory authority in the US anyway

>> No.14857078

>>14857072
lest it showeth the four corners of the earth, (Job 37:2–3, ESV)

>> No.14857093

>>14857072
Well I don't know what the fuck Astra was doing with their 4ASS tier cameras then.
>buy a bunch of cheapass IP cameras literally on Amazon
>strip them and put them in custom housings
>attach to rogget
>configure
Whatever regulation exists must be feather light for stuff strapped to rocket stages.

>> No.14857095
File: 23 KB, 786x800, apollo 4 Earth as Viewed From 10,000 Miles.jpg [View same] [iqdb] [saucenao] [google]
14857095

>This chapter describes the talmudic model of the universe. The rabbis of the Talmud believed that the world was flat, and that the sun revolved around the Earth every day. There is a debate about the length of the solar year in the Talmud, and its consequences and the rare Jewish ceremony of the Blessing of the Sun (Birkat Hahammah) are discussed. The view of the talmudic rabbis is contrasted with that of the contemporary Greek astronomers. While the rabbis of the Talmud argued about the size of the flat Earth, the Greeks had determined the Earth to be a sphere, had calculated its circumference and had moved on to consider other questions.
https://academic.oup.com/book/1751/chapter-abstract/141387578?redirectedFrom=fulltext

>> No.14857102
File: 89 KB, 587x885, orbital station tatsushi morimoto jinsei choh.jpg [View same] [iqdb] [saucenao] [google]
14857102

>> No.14857103

>>14857095
apparently they also believed the whole Earth was flooded at one point

>> No.14857105

>>14857072
How are they defining spacecraft for that? What about a camera taken to a permanent moon base?

>> No.14857119

>>14857105
I'm basing this off of https://www.nasa.gov/sites/default/files/atoms/files/nasa_csli_cubesat_101_508.pdf
>if you have a non–Federal Government CubeSat with any type of active or passive imager, you must obtain a remote sensing license from NOAA’s Commercial Remote Sensing Regulatory Affairs (CRSRA).

https://www.nesdis.noaa.gov/about/our-offices/commercial-remote-sensing-regulatory-affairs
>The National and Commercial Space Programs Act (NCSPA or Act), 51 U.S.C. § 60101, et seq as amended (the Act), provides no person who is subject to the jurisdiction or control of the U.S. may operate any private remote sensing space system without a license, and authorized the Secretary of Commerce to license private sector parties to operate private remote sensing space systems.

>> No.14857121

>>14857072
this is false
>inb4 links to a news article

>> No.14857122

>>14857072
Big brain, this is why Russia is doing so bad, the US won't let them launch spy satellites.

>> No.14857123

>>14857093
I think it's more about not having people put their own spy satellites up.

>> No.14857126

>>14857119
>everything requires a license
I hate the government so much.

>> No.14857129

>>14857123
reconnaissance should be for everyone not just the government

>> No.14857132
File: 535 KB, 3356x4063, FPxANllXsAEMktP.png [View same] [iqdb] [saucenao] [google]
14857132

looks like a 5G tower desu

>> No.14857135

>>14857126
Makes sense seeing they don't want 4ASS pointing a spy satellite at their submarine pens, if you don't like it you can leave the land of the free and get more freedom.

>> No.14857137
File: 370 KB, 3588x3844, FPxAaZsXsAIliNp.png [View same] [iqdb] [saucenao] [google]
14857137

>>14857132

>> No.14857139

>>14857129
That doesn't mean that they'd force Astra to buy better cameras.

>> No.14857141

The US government also limits the resolution of commercial imagery satellites.

>> No.14857143

>>14857132
>>14857137
>@TwitterFaggot
>it occured to me in a dream

>> No.14857146

>>14857095
They really just get more and more schizophrenic and insane the more you read about them, huh?

>> No.14857147

>>14857103
That's what i would think too if I saw fish fossil up in the mountains.

>> No.14857153

>>14857146
Yeah. Greeks were crazy, I can't believe they thought they knew better than G-d

>> No.14857154

>>14857141
Eventually that won't matter because someone else will provide it, then everyone will need to work underground to avoid them.

>> No.14857156

>>14857146
There's a reason we don't name planets after their mythology.

>> No.14857157

>>14857147
Never thought about that but yeah, if you know nothing of tectonic plates and find sea shells and fish on top of mountains clearly the flood was at least that high.

>> No.14857158

>>14857135
Everyone who cares about the sub pens is a foreign government with its own spy satellite program. This is just about the federal government putting a tax on every possible economic activity in order to support the bureaucrats that are obviously needed to ensure compliance with licensing regulations.

>> No.14857169

>>14857158
>Everyone who cares about the sub pens is a foreign government with its own spy satellite program
You really think Myanmar has a spy sat network? I know that commercial providers like google and bing get given coordinates to sensor because there are a fuckload of people without their own spy sats that would like to know where things are.
A really simple case is ISIS using it for military recon, they have the money and need but the US government won't let them launch from the US.

>> No.14857172

>>14857157
And dragons and rocs was just dinosaur bones

>> No.14857181

>>14857137
inb4 they fail to deploy

>> No.14857188

>>14857147
yeah and skeletons of dragons under the dirt

>> No.14857192
File: 131 KB, 3622x2498, Fc9Fa_iWQAAIv37.png [View same] [iqdb] [saucenao] [google]
14857192

apgee guy did a thing

>> No.14857197

>>14857192
>propulsive landing
I'm curious to see this in action. NASA didn't go for this for some reason on Dragon

>> No.14857201

>>14857146
you haven't read anything
Deuteronomy 28:53-63

>> No.14857202

>>14857192
sussy

>> No.14857209

>>14857169
You really think Myanmar is all that interested in talking high resolution pictures of Norfolk?

Washington is free to put whatever sanctions it want onto ISIS and everyone associated with them. They already have They did the same to Russia and they'll do the same to anyone else who's on the wrong side of one of our geopolitical contests. It's a separate and unrelated issue from the government's ongoing desire to continue robbing its citizens under the pretext of needed to better manage their lives for them.

>> No.14857210

>>14857202
baka

>> No.14857212

>>14857192
nothing positive to say about that esa cuckpod. relativity will eat their lunch 50 times over

>> No.14857215

>>14857197
NASA were too conservative to commit to the idea for crew launches and SpaceX's Mars plans evolved past the use of dragon capsules pretty quickly.

>> No.14857217

I unironically think propulsive landing for screw dragon is a bad idea that would end in disaster sooner or later.

>> No.14857218

I like Susie because of her cute name.

>> No.14857225

>>14857197
They wouldn't sign off on it for crew and SpaceX didn't want to be running 2 different designs so removed it from cargo too.

>>14857209
>You really think Myanmar is all that interested in talking high resolution pictures of Norfolk?
No but I think they want to find where the Karen are hiding in Myanmar, you see satellites can see anywhere on earth depending on orbit. The IRA can use then in Ireland, Hezbollah can use them in Israel ect.
Falling costs means any group that can raise ~$200k can get a decent camera into orbit, they just can't launch it from the US because of this law.
>everyone associated with them
How do you know everyone that is associated with them?

>> No.14857232
File: 9 KB, 209x241, 1459984625101.jpg [View same] [iqdb] [saucenao] [google]
14857232

>>14857201
wtf

>> No.14857236
File: 236 KB, 1200x711, Now that's what I call a rocket girl.jpg [View same] [iqdb] [saucenao] [google]
14857236

https://twitter.com/maxNSFWshroom/status/1571190361598447616

>> No.14857241
File: 24 KB, 534x443, 1358442223434.jpg [View same] [iqdb] [saucenao] [google]
14857241

>>14857217
>screw dragon

>> No.14857248

>>14857201
>>14857232
>you will eat the afterbirth
Those bugs are starting to sound pretty good in comparison.

>> No.14857249

>>14857225
Hezbollah is under sanctions like all the rest of the people on the bad actors and terrorists list. The IRA haven't been a thing for years. The government of Myanmar is either already on the bad actors list, in which case you can't sell satellite data to them, or they're not, in which case the US government doesn't give a shit about whatever bloody internal politics are going on in the country.

The US government is very good at figuring out who is doing business with who. It's the same intel they use everyday to decide if there's something going on that they can justify taxing.

>>14857236
And apparent this is a completely different guy from the last guy who was drawing erotic anthro spacecraft art

>> No.14857256

>>14857192
crew dragon can carry 7 people tho

>> No.14857258

>>14857249
>The US government is very good at figuring out who is doing business with who
Remind me why does Iran have F-14s? Why were the US worried about US made stingers in Afghanistan?
Politics are always changing and the US is the best in the world at arming and training future enemies. I know you want to cry "gubment bad" and bitch about regulations but the reality is stopping privately owned spy satellites is a good idea, I hope they inspect all satellites because some Uncle Ted wanna-be sending up a ball bearing dispenser could start Kessler syndrome.

>> No.14857262

>>14857258
>I hope they inspect all satellites because some Uncle Ted wanna-be sending up a ball bearing dispenser could start Kessler syndrome.
made me chuckle, anyway, accelerate

>> No.14857279
File: 146 KB, 933x550, firefox_2022-09-18_15-41-28.png [View same] [iqdb] [saucenao] [google]
14857279

>to fly
Come again?

>> No.14857282

>>14857279
>not the R-7
>not the Falcon
>the fucking SLS
Do you only follow him because he says really dumb things?

>> No.14857285

>>14857279
Kek what happens when the engine fails shortly after abort tower jettison?

>> No.14857286

>>14857285
Did they seriously leave a gap between abort modes after the space shuttle?

>> No.14857287

>>14857258
Iran has F-14s because they stole them from the Shah. Good luck doing that with an American operated satellite in LEO. And we were worried about stingers in Afghanistan because some of the people that Washington itself was selling to turned out to be less than reputable. That's the sort of thing that happens when you assume that all jihadis are trustworthy allies just because they're fighting someone else you don't like. That was not and never was the fault of private American citizens and the idea that further regulation of the American people would have prevented it is wild.

There is no reason for the government to demand a tax for satellite imagining capability. Every issue that is brought up to justify this is already covered by another preexisting form of government regulatory power. The only reason this exists is for the mother-may-I state to continue to demand payment for the undertaking any economic activity. Regulators only exist to enforce rules that ensure their continued comfortable employment. Taxation is theft.

Also kessler syndrome isn't real.

>> No.14857294

talking of space cameras...
https://twitter.com/RGVaerialphotos

>> No.14857298

>>14857282
>follow him
this is a screenshot of a twitter screenshot so I'm at least twice removed from him, ver based

>> No.14857300
File: 133 KB, 858x737, frogworks.png [View same] [iqdb] [saucenao] [google]
14857300

>>14857192
Ariane just clapped back at whole spaceflight industry, hot damn

>> No.14857304

>>14857285
>>14857286
There is no problem with engines failure, the orion just separates and flies away with the AJ-10.
If however orange tank or the ICPS explodes after SRB & escape tower jettison then there's a good chance the capsule can't get away fast enough and gets damaged.
This is why Dragon is arguably the safest capsule from an abort standpoint at least.

>> No.14857308

>>14857304
lmao so that Mike guy doesn't know what he's talking about then

>> No.14857317

Why dont airplanes have catch towers? no need for wheels

>> No.14857322

>>14857304
Why can't the just do it the way the Russians have been since '66? Wait for burnout and seperation of the stage that puts you on a safe sub-orbital trajectory and then ditch the tower.
There is no point in a saw-yooz launch where you don't have the tower or safe reentery.

>> No.14857325

Prepare for staging

T-Minus

>> No.14857329

>>14857325
No clearance from the FAA has been granted - ABORT

>> No.14857333

>>14857322
That is exactly what is happening here too. Reread the post.

>> No.14857339

>>14857333
Ah, yeah if the final insertion stage explodes you are dead, I can't see a way around that one.

>> No.14857341

>>14857339
The way around that is the Dragon escape system. It goes all the way to orbit.

>> No.14857352

>>14857341
True but now you have a hypergolic engine and tanks in the capsule which I would argue poses a greater risk of explosion than a hydrolox stage you only ride for a few minutes.

>> No.14857358

>>14857014
Jet fuel is less refined, but RP-1 is very highly refined, as even a tiny amount of sulfur in the fuel fucks up the engine rapidly.

>> No.14857360

>>14857025
For an expendable rocket, yeah. For reusable rockets the fuel cost becomes significant the better you get at reusability, so a cheaper fuel is generally better as long as it doesn't cut performance horrifically.

>> No.14857362

>>14857037
Yes it's not linear, but they're still better. Look up the S1.5400, a staged combustion kerolox engine from 1960 with better thrust to weight ratio than the modern RL-10. Yes kerolox offers an inherent TWR advantage, but so does 60+ years of materials science and manufacturing improvements.

>> No.14857371

>>14857055
>At this point a methalox engine with >=380s Isp beats hydrolox every time just for simpler tanking and better overall delta-V.
This is true unless your system is mass limited instead of volume limited AND you have no access to on-orbit propellant transfer. That is to say, a 100 ton methalox stage will get less payload to X orbit than a 100 ton hydrolox stage. However, since propellant transfer is about to become industry standard before 2030, this point is irrelevant. Hydrolox will only make sense as a propellant of convenience once we are operating in such places as the gas giant moons, where water is hyperabundant and carbon not so much, plus the delta V requirements to anywhere are low anyway and the difficulty of thermally insulating the hydrogen form the environment is greatly reduced due to the lower solar influx.

>> No.14857376

>>14857095
>While the rabbis of the Talmud argued about the size of the flat Earth, the Greeks had determined the Earth to be a sphere, had calculated its circumference and had moved on to consider other questions.
based greeks

>> No.14857384

>>14857132
>measuring power in units of area

>> No.14857391

>>14857192
>40 m^3 (pressurized)
that's a filthy lie

>> No.14857392

>>14857384
It's about 36 liters if that helps.

>> No.14857398

>>14857258
>the reality is stopping privately owned spy satellites is a good idea
Wrong

>> No.14857400

>>14857352
>hypergolic engine and tanks in the capsule which I would argue poses a greater risk of explosion
Attempt to prove this

>> No.14857403

>>14857400
https://youtu.be/xe4ee56aHSg

>> No.14857406

>>14857371
Spacecraft at the gas giant moons need nuclear heat and power anyways so even then it'd be a Triton engine (bimodal LANTR) rather than true hydrologgs chemical.

>> No.14857407

>>14857403
This is why we do unmanned tests, that failure mode is now impossible. Try again?

>> No.14857413

>>14857407
Show me a Centaur exploding, not because the lower stages did but because the centaur did, it's been flying 60 years so surely you can find one.
The fact is if your fuel and oxidizer mix you have the potential for an explosion but still need an ignition source, unless they are hypergolic like the SuperDraco's in which case as soon as they touch it's going off.
If you don't understand that hypergolic's are higher risk than hydrolox there is no point trying to talk to you about rocketry.

>> No.14857419

>>14857418
>>14857418
>>14857418

New thread

>> No.14857424

>>14857406
Your premise is flawed (solar at Jupiter and Saturn is still viable, if increasingly cumbersome, and what heat sources are needed in compact form would need to be on the scale of kilowatts at most, not gigawatts like the typical NTR reactor.
Regardless, what I'm talking about is, for example, a vehicle which launches off of Callisto to an equatorial orbit, drops off payload, then deorbits and lands propulsively, all in a single stage and as often as multiple times a day (depending on propellant availability). Nuclear thermal engines have their use cases but for surface to orbit shuttles they're very difficult to turn around rapidly because of the short lived fission products lingering after shutdown and blasting everything around the engine with gamma rays. Also, NTR has
a much lower thrust to mass ratio which means the propellant load and payload mass are limited severely by what the engines can actually lift, making NTR not a good choice for launching anyway. It's like the methalox vs hydrolox booster argument all over again, except in this case hydrolox is the more convenient and higher impulse density propellant choice.

>> No.14857426

>>14857413
Centaur doesn't perform launch abort, silly.

>> No.14857434

>>14857426
But you are saying the risk of SLS abort is the Centaur exploding.
I found this by the way, first ever flight of Centaur and it blew.
>On May 8, 1962, the first Centaur rose, a perfect launch for the first 54 seconds. Then, the Centaur upper stage exploded.
https://www.nasa.gov/centers/glenn/about/history/centaur.html

>> No.14857444

>>14857434
>But you are saying the risk of SLS abort is the Centaur exploding
not the same person

>> No.14857448

>>14857444
So what are you arguing then? That hypergolics aren't inherantly higher risk than conventional fuels?

>> No.14857452

>>14857362
Yes, I know about the S1.5400. I use it for some interplanetary missions in KSP RSS even, but material science has not evolved too much in regards to rocket engines, or at least to in making them less heavy. The material science that has evolved since then is more about alloys being able to handle hot oxygen better and changes to the metallurgy processes. And in regards to manufacturing it has become cheaper, faster and require less parts but not necessarily better performance. You still have engines designed and produced in the 60's that mog pretty much any engine today besides the Raptor (like NK-33, RD-57 and RD-270 to mention a few).

For a modern example Rocket Factory Augsburg has made a kerolox ORSC engine named Helix at 100kN, but its pretty heavy for that class iirc.

>> No.14857456

>>14857434
SLS doesn't have a centaur, and also, I never said that. You're talking to multiple anons.
As for proven track records, the Ariane 4 flew 116 times and suffered 3 failures, of which only one had anything to do with the hypergolic main engines, and was in fact the result of a man leaving a handkerchief inside the engine rather than anything to do with propellants leaking or otherwise a result of the use of hypergolics.

>> No.14857467

>>14857452
>but material science has not evolved too much in regards to rocket engines
You silly billy.
Anyways SpaceX has shown that there are huge TWR gains to be made in two engine cycles (gas generator and FFSC) compared to the rest of the industry, through iterative design approach. However, I strongly doubt there are similar TWR performance gains to be made in the RL-10 simply because the engine's performance is limited by how much heat can be conducted through the chamber and nozzle walls per mass unit of propellant.
I guess I should amend my original point and say I want SpaceX to build an RL-10 killer and sell it to everyone, because their track record indicates that they could.

>> No.14857486

>>14857456
I'm basing the risk on Centaur because the ICPS is basically a DCSS which is Centaur derived.
I did find https://www.flightglobal.com/delta-iii-engine-exploded/27511.article
which is an RL-10 cato taking out a DCSS making 2 RL-10 stages causing the issue in 60 years of flight.

>> No.14857675

>>14857192
Why does apogee include Susie but not crew starship, considering crew starship will probably be a thing well over a decade before susie is?

>> No.14857717

>>14857232
Read all of the chapter and you will see its taken out of context. At least 15-68 as its intended.

Still weird but less weird when read as intended.