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2023-11: Warosu is now out of extended maintenance.

/sci/ - Science & Math


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11489376 No.11489376 [Reply] [Original]

old thread >>11480402

>> No.11489384

>>11489376
>guys only want one thing and it's fucking disgusting

>> No.11489397

>>11489384
>what's that, sex?

>> No.11489398
File: 1.47 MB, 762x1125, my_ideal_future.png [View same] [iqdb] [saucenao] [google]
11489398

>>11489384
>>11489397

>> No.11489406

>>11489397
Starship

>> No.11489421

You're probably right. OneWeb is fucked and nobody is going to buy them out, especially now that we're in a corona recession.

>> No.11489434

>>11489421
I literally called it

>> No.11489471

HULLO
https://www.youtube.com/watch?v=V7e-1bRpweo

>> No.11489491

>>11489421
but they are going to launch in less than an hour anyway?! I guess it is too late to cancel the launch contract or something?

>> No.11489501

>>11489491
I don't know how it works out either. Maybe they're trying to keep it going as long as possible while praying that some sucker buys them out?

>> No.11489523
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11489523

we gonna break 150 launches this year?

>> No.11489531

>>11489501
>Maybe they're trying to keep it going as long as possible while praying that some sucker buys them out?
Probably this, though they might be trying to buy some time, since filing for bankrupcy isn't as simple as it sounds

>> No.11489532

>>11489523
maybe

>> No.11489537

>>11489523
no. Even in a typical year, a large chunk of scheduled launches are delayed. But with the economic crash and Corona shutdowns, a whole bunch more are going to be delayed or canceled. India has suspended all launch operations, for example, and ESA has shut down their Kourou launch site.

>> No.11489541

>>11489523
what are the red from this year?

>> No.11489544

>>11489541
failures

>> No.11489553
File: 178 KB, 946x946, OneWeb-L3-Mission-Patch.png [View same] [iqdb] [saucenao] [google]
11489553

https://www.youtube.com/watch?v=bg3ffqkef6w
OneWeb launch stream

>> No.11489564

>>11489544
which rockets failed, anon

>> No.11489575

>>11489564
january iranian simorgh
march chinese long march 7

>> No.11489577

>>11489575
does a ballistic missile test really count as a launch vehicle failure

>> No.11489579

>>11489577
it was carrying a satellite

>> No.11489581

>>11489579
oof

>> No.11489614

>>11489553
successful launch so far, Fregat coast phase now

>> No.11489643

>>11489553
So they basically retranslated Roscosmos stream.

>> No.11489656

>>11489471
lol i just saw that

>> No.11489683
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11489683

>> No.11489690
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11489690

fuck Roskosmos
fuck OneWeb
and most importantly
fuck SLS

>> No.11489693
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11489693

>>11489471

>> No.11489695

more stacking has occurred

>> No.11489698

>>11489693
what happens if you jump in that

>> No.11489700
File: 95 KB, 1280x720, 897cc0b3beadee5e342a2075dc8ef7f9.jpg [View same] [iqdb] [saucenao] [google]
11489700

>>11489695
I REQUIRE EVIDENCE OF THE
S T A C C

>> No.11489702

>>11489698
you punch yourself in the balls

>> No.11489725
File: 732 KB, 1536x2048, 0B72549C-B57C-4A16-A9F5-887F21550206.jpg [View same] [iqdb] [saucenao] [google]
11489725

On the road again...

>> No.11489758

Where are all of the entry level manufacturing jobs at Boca Chica? How do you get hired there without a ton of specialized experience?

>> No.11489759

>>11489758
Lol you expect a cheapskate like musk to train people?

>> No.11489764

>>11489759
For something like this? Yes.

>> No.11489768

Nevermind, found one or two I qualify for. Gonna apply, wish me luck.

>> No.11489772

>>11489768
Good luck. Send pics when you make it.

>> No.11489792

>>11489698
death

>> No.11489797

>>11489758
Apparently a lot of the people there have experience in welding and shit from the oil industry

>> No.11489798

>>11489471
>Now, it looks flat-ish. Because when you're close to a sphere then it looks like a flat object.
Shots fired.

>> No.11489860
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11489860

S T A C C

>> No.11489911
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11489911

>> No.11489917
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11489917

>> No.11489920

>>11489917
>>11489911
was it successful?

>> No.11489922
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11489922

>> No.11489924
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11489924

>> No.11489930

>>11489920
We don’t know yet, 6 of the satellites are confirmed to have separated. It takes a couple hours to deploy them all because they spread them out.

>> No.11489939

>>11489860
Rivets now?

>> No.11489944

>>11489939
no, those are the heat affected zone discoloration from the internal stiffeners
that's the aft skirt

>> No.11489962

>>11489939
Internal spot welds
A bunch of stringers go in the un-pressurized barrel sections for additional support with minimal additional weight.

>> No.11489999
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11489999

>> No.11490097

i dont think spacex has a week anymore. expect statewide lockdown soon.

>> No.11490098

>>11489398
I want it so bad bros.

>> No.11490126

>>11490097
Shut up FUD poster. SpaceX is fine.

>> No.11490132

>>11489999
Is that the rocket that can separate the engines and recover them by parachute/helicopter?

>> No.11490136

>>11490132
there's plans for doing that "eventually" but now that they're buying BE-4 it probably isn't worth it

>> No.11490149
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11490149

>>11490136
>there's plans for doing that "eventually"

There’s definitely plans to do it, they just have to wait until 2022 to start working on it because that’s when LOFTID, which is essentially a proof of concept for SMART will be launched and tested.

https://www.nasa.gov/feature/goddard/2019/inflatable-decelerator-will-hitch-a-ride-on-the-jpss-2-satellite

>> No.11490155

>>11490149
Aka no such plans because nasa isn’t going to give them a contract for it

>> No.11490165 [DELETED] 
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11490165

>>11490155
>The Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID) is a public-private partnership between NASA’s Space Technology Mission Directorate and United Launch
Alliance (ULA). The LOFTID project is poised to revolutionize the way NASA and industry deliver payloads to a planet’s surface or into orbit, utilizing aerodynamic forces instead of propulsion. Since NASA’s inception in 1958, the agency has relied heavily on retro-propulsion (rockets) and rigid heat shields to decelerate people, vehicles, and hardware during orbital entry, descent, and landing (EDL) operations.
After more than a decade of development
of the Hypersonic Inflatable Aerodynamic Decelerator (HIAD) technology, including two suborbital flight tests, the LOFTID orbital flight test is the next logical step. Return from orbit provides an entry environment relevant to many potential applications, paving the way for its use on future missions. HIAD technology can enhance, and even enable, larger missions to higher elevations at Mars. It can also be applied at Earth, providing capability for International Space Station (ISS) down-mass, or even enabling return for free-flying orbital manufacturing. Recovery of spent launch vehicle assets for reuse, such as ULA’s plan to recover their first stage booster, can reduce the overall cost of access to space.

https://www.nasa.gov/sites/default/files/atoms/files/loftid_fact_sheet_june2019.pdf

>> No.11490171 [DELETED] 
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11490171

>>11490155
https://www.nasa.gov/sites/default/files/atoms/files/loftid_fact_sheet_june2019.pdf

>The Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID) is a public-private partnership between NASA’s Space Technology Mission Directorate and United Launch
Alliance (ULA).

>> No.11490176
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11490176

>>11490155
https://www.nasa.gov/sites/default/files/atoms/files/loftid_fact_sheet_june2019.pdf

>The Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID) is a public-private partnership between NASA’s Space Technology Mission Directorate and United Launch Alliance (ULA).

>> No.11490191

>>11490165
>>11490171
>>11490176
Wha has this to do with turning “smart” into a reality?
Nothing, it’ll never happen

>> No.11490206

>>11490191
>Wha has this to do with turning “smart” into a reality?
>Nothing, it’ll never happen

>The LOFTID Reentry Vehicle (RV) is a secondary payload hosted on an Atlas V launch vehicle, and will be delivered to its reentry state by the Centaur, the Atlas V second stage. The RV is stowed within a primary payload adapter on the Centaur, such that the primary payload adapter can be released and separated to expose the stowed aeroshell for deployment while the RV is attached to the Centaur. The RV is inactive and powered off during the launch and delivery of the primary payload. After the primary payload has been delivered to orbit, the Centaur performs a deorbit burn to reenter the Earth’s atmosphere. After the payload adaptor is jettisoned, the RV is then powered on, the packing restraint is released, and the aeroshell inflation is initiated. The inflation system begins a “soft start” and then full inflation, delivering nitrogen inflation gas from pressurized tanks provided by ULA. When the aeroshell is fully inflated, the Centaur attitude control system spins up the spacecraft and performs a final pointing adjustment before releasing the RV on its spin-stabilized reentry trajectory. The Centaur then performs a divert maneuver to avoid re-contact with the RV as the Centaur burns up on reentry. The RV reenters the atmosphere on the prescribed trajectory, and decelerates from hypersonic down to subsonic flight. Throughout the RV flight, a real-time beacon transmits minimal data packets to a satellite network, while data from instrumentation, cameras, and other subsystems is acquired and processed, sending duplicate comprehensive data to both an Internal Data Recorder (IDR) and an Ejectable Data Recorder (EDR). After reentry, the RV ejects the EDR, which is buoyant and provides a GPS locator signal for physical recovery from the ocean surface.

>> No.11490225

>>11490206
So 2 years from now they will do a balloon test with hardware totally unrelated to anything else

This is just some technology demonstrator which is one of the ways NASA turns a project that should only last a year into 2 decades of research and a billion dollars

>> No.11490257

>>11490225
>So 2 years from now they will do a balloon test with hardware totally unrelated to anything else

It’s literally a full-scale re-entry test for the inflatable heat shield SMART will use, stop with the mental gymnastics.

>> No.11490296

>>11490225
Come on man. NASA deserves alot of shit for their management, but you're reaching there.

>> No.11490304
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11490304

See you niggers later. I'm gonna go to Mars in like five days on my shear flow stabilized fusion rocket

https://www.sciencedirect.com/science/article/abs/pii/S0094576509001556

>> No.11490305

>>11490304
ah yes, the classic direct energy converter

>> No.11490306

>>11490149
>wait until 2022 for the proof of concept
>2023 for design
>2024 for flight test
>2025 for improved flight test
>2026 for first production version almost finished
>whoops first production version slipped to 2027
>first flight of the hardware in 2028
Now to start designing that helicopter...

>> No.11490315

>>11489421
Bezos buys OneWeb when? He could probably get them for pennies on the dollar the way the world economy is right now.

>> No.11490341

>>11490306
This is a ULA project and their pretty good at keeping to schedules, so your worries are likely unfounded.

>> No.11490350

Bros suggest me a book to read, not a textbook but also not a book about the history of rockets or something like that

>> No.11490361

>>11490315
Beaks doesn’t have the money nor does he have any launch vehicles

>> No.11490375

>>11490361
>nor does he have any launch vehicles
yet

>> No.11490390

>>11490257
>>11490296
But it isn’t, it’s just some small scale 6 meter demonstrator, which “can be scaled in the future”

ACES is not going to happen and neither is SMART
Their long term future plan is just to declare bankruptcy and retire

>> No.11490405

>>11490390
Centaur V has many of the ACES upgrades baked in, like the hot gas-gas RCS thrusters and such

>> No.11490419

>>11490390
>But it isn’t, it’s just some small scale 6 meter demonstrator, which “can be scaled in the future”

LOFTID is 6 meters in diameter, which is wider than Vulcan’s 5.4 meter core. NASA have stated it can be scaled up, and their correct, LOFTID itself is just a scaled-up version of earlier, smaller inflatable heat shields that have been tested, so why not scale up more in the future?

>> No.11490426

>>11490405
I’m pretty sure they plan to phase ACES’ IVF technology (which is the only thing CV is lacking) in as part of the NSSL Phase 3, which is all about “new capabilities”.

>> No.11490431

>>11490426
and then the only difference between Centaur V and ACES will be the insulation for indefinite cruise time

>> No.11490437

>>11490419
wait, this isn't a new technology they're demonstrating? it's just the latest in a series of progressively larger prototypes?

>> No.11490438

>>11490431
Yes and that

>> No.11490443

>>11490419
Inflatable reentry vehicles is nothing new, if they were serious about it then they wouldn’t be waiting for demonstrators and after their rocket starts launching

Instead the plan would be to always recover engines

>> No.11490452

>>11490437
>it's just the latest in a series of progressively larger prototypes?

>NASA launched an inflatable heat shield experimental spacecraft on 17 August 2009 with the successful first test flight of the Inflatable Re-entry Vehicle Experiment (IRVE). The heat shield had been vacuum-packed into a 15-inch-diameter (38 cm) payload shroud and launched on a Black Brant 9 sounding rocket from NASA's Wallops Flight Facility on Wallops Island, Virginia. "Nitrogen inflated the 10-foot-diameter (3.0 m) heat shield, made of several layers of silicone-coated [Kevlar] fabric, to a mushroom shape in space several minutes after liftoff." The rocket apogee was at an altitude of 131 miles (211 km) where it began its descent to supersonic speed. Less than a minute later the shield was released from its cover to inflate at an altitude of 124 miles (200 km). The inflation of the shield took less than 90 seconds.

>Following the success of the initial IRVE experiments, NASA developed the concept into the more ambitious Hypersonic Inflatable Aerodynamic Decelerator (HIAD). The current design is shaped like a shallow cone, with the structure built up as a stack of circular inflated tubes of gradually increasing major diameter. The forward (convex) face of the cone is covered with a flexible thermal protection system robust enough to withstand the stresses of atmospheric entry (or reentry).

>In 2012, a HIAD was tested as Inflatable Reentry Vehicle Experiment 3 (IRVE-3) using a sub-orbital sounding rocket and worked.

>In 2020 there were plans to launch in 2022 a 6 m inflatable as Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID)

>> No.11490459

>>11490305
better then a Stirling Engine

>> No.11490477
File: 2.56 MB, 1081x609, niac_spear1_0.png [View same] [iqdb] [saucenao] [google]
11490477

https://www.nasa.gov/directorates/spacetech/niac/2019_Phase_I_Phase_II/SPEAR_Probe

New nuke proposals have arrived. What do you fags think of this?

>> No.11490497

>>11490350
Slaughterhouse Five.

>> No.11490498
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11490498

>>11490477
First of all, this proposal is a year old, secondly it uses Nuclear Electric Propulsion..., third and finally it’s a NIAC, meaning it’s basically just a futuristic study. An actual nuclear mission to get excited about is whatever NASA and the Department of Energy are currently working on with actual funding.

>> No.11490513

>>11490498
>non chemical or ionic propulsion
>happening with NASA

>> No.11490522

>>11490513
You’d be right up until now, considering NASA hasn’t had funding to develop nuclear propulsion since the 1960s until 2019. Also, who else but NASA will the government allow to put fissile material on a rocket? There’s currently only a single US rocket allowed to carry nuclear material, even in the form of RTGs.

>> No.11490530

>>11490498
K, but ignoring all that, the real prize from that proposal is the lithium deuteride moderated low-enriched-uranium fuel reactor.

Kilopower would be great but it's reliant on high enriched uranium, weapons grade enrichment in fact. That's never going to be something easy to draw into mission plans because the fuel is so politically touchy to even talk about. Low enriched fuel on the other hand is manufactured in the thousands of tons per year, there's no issue with that.

>> No.11490542

>>11490530
Direct nuclear propulsion will be much easier once colonies independent of any earth government are formed.

>> No.11490555

>>11490542
Of course, but I want my nuclear powered flagship class Uranus and Neptune probes NOW god dammit

>> No.11490594
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11490594

>> No.11490678

>Elon Musk and Jeff Bezos want "$5 billion in grants or loans to keep commercial space company employees on the job and launch facilities open." They also want the IRS to give them cash for R&D tax credits.

https://twitter.com/matthewstoller/status/1241446042232594434

>> No.11490688

>>11490678
based
I hope they get it, but probably not

>> No.11490701

>>11490678
Elon deserves it
Bezos' whole shtick up to now has been his unlimited bank account, so what gives?

>> No.11490703

>>11490688
Yeah, probably not considering their both multi-digit billionaires (so them getting financial aid is laughable) and the Democrats are limiting the corporate bailout to $150 billion to be split up between the industries, there’s different sectors who are far more in need of this money.

>> No.11490704

>>11490678
We should have given them the 1.5 trillion that the stock market got for its bailout.

>> No.11490714

>>11490703
If I have $10 in my bank but I manage a company worth $10 trillion. If I ask for $10000000000000000000000000 trillion, the government should give me money for my company because I'm poor? What does someone's networth have to do with getting loan for their companies? lol

>> No.11490728

>>11490703
it's less about their personal wealth and more about commercial spaceflight not being crucial for our national infrastructure

>> No.11490738

>>11490728
wrong

>> No.11490752

>>11489725
What is that?

>> No.11490773

>>11490703
Uh mate just because you have a 50% stake in a large company doesn’t mean you magically have billions in liquid cash to burn on non profitable things

>> No.11490783

>>11489758
>wants entry level job
>welding spaceships
Piss off zoomer, go back to college, you aren't special.

>> No.11490796

>>11490703
>Yeah, probably not considering their both multi-digit billionaires (so them getting financial aid is laughable)

Giant corporations and billionaires get the most financial aid in the US

>> No.11490800

>>11490752
Casket for SLS employees who got coronavirus

>> No.11490802

>>11490783
Someone is salty.

>> No.11490812

>>11490375
>yet
Its been "yet" for years. I'm hopeful for BO, but holy hell they need to show some advancement. They have photos of fairings and complete engines, but nothing functional.

>> No.11490823

>JWT devolpement halted due to corona
HOW COULD THIS HAPPEN TO ME!
I MADE MY MISTAKES
I

>> No.11490826

>>11490802
Nope, I hate kids that get upset over companies not hiring and training them. Go read a book and train yourself at a minimum. Don't cry on the internet that you can't get paid to learn a skill.

>> No.11490872
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11490872

THE SOVIET BVLL

>> No.11490877

>>11490826
Corona chan is coming for your lungs boomer scum

>> No.11490881

>>11490826
Meanwhile the boomer would never in a million years hire a “self trained” guy in his 20s

>> No.11490883
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11490883

>> No.11490894

>>11490883
I like Elon in general but it's pretty obvious he's trying to calm panic to keep his stonks up which I think is a gassable offense.

>> No.11490905

>>11490883
>Nooo, not muh stonkerino

>> No.11490914

If we did colonize the moon and a plague similar to Coronavirus happened, would the moon colonists be stuck in the moon until a vaccine was made?

>> No.11490919

>>11490894
Panic is for retards. Stocks actually matter, unlike Coronavirus killing some boomers.

>> No.11490945

>>11490914
VENT
OUT
AIRLOCK

>> No.11490953
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11490953

>> No.11490985

>>11490914
You could sterilize stuff on the moon by leaving it outside for a bit.

>> No.11490995

>>11490985
Sick people too.

>> No.11491004

>>11490914
>Be Moon colonist
>Did you hear about the plague on earth?
>Earth? Lmao I don't give a fuck about Earth

>> No.11491007

>>11490985
>>11490945
>>11490995
Just put them in the airlock and pump it down to near vacuum to evaporate off all the moisture. Viruses are killed by being dried out, so if you just dry the infected into jerky you now only completely disinfect them you also increase your food supply by a few dozen kilos per body

>> No.11491010

>>11491007
Very grimdark. I like it.

>> No.11491077

>>11490872
>explodes

>> No.11491099

>>11491077
:(

>> No.11491106

>>11490872
if korolev hasnt died and if they had went with a soyuz mission assembled in earth orbit wed be speaking russian now,

also wed have reusable energia boosters by now. the buran was notably superior to the shuttle.

one could take off automated from the harshest climate on earth and the other could explode if the weather was 1 degree below the average in florida, oh and it needed to have people to kill or it wouldnt take off

>> No.11491109

>>11490883
elon musk is obviously a savant autist, incredibly capable for some things, borderline retarded for others

>> No.11491132

>>11491106
This is probably the stupidest post I've ever read

>> No.11491135

>>11491132
It's not even the stupidest post I've read today.

>> No.11491194

>>11491132
I don't know anon, I've read a lot of flat earth posts today.

>> No.11491301
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11491301

>>11489384
All I'm hoping, and praying for, is for the James Webb Space Telescope to explode on the launchpad in the year 2030 after all the useless fucking delays

>> No.11491311

>>11491301
That would be hilarious.

>> No.11491318

>>11491301
And that rocket will be the inaugural mission of the SLS.

>> No.11491320

>>11491318
no, it's launching on an Ariane rocket

>> No.11491322

>>11491320
What? Why?

>> No.11491323

>>11490953
we havent seen any legs right? maybe sn3 wont have them...

>> No.11491324

>>11491322
government

>> No.11491338

how do you get nuclear into space anyway? is it through the doe? we're going to need nuclear as baseline power for any colonies, especially lunar.

>>11490594
whats this?

>> No.11491344

>>11491338
looks like Blue Origin's Florida pad

>> No.11491347

>>11491338
You suck Terran dicks until you get nicknamed Black Vortex and beyond, establishing a robust and well-supplied colony with everything except raw materials manufacturable on-site. Then you start shifting more and more personally/colonially owned resources into asteroid prospecting and mining.

>> No.11491352

>>11491338
>how do you get nuclear into space anyway?
Kick every ethnic chink out of the country and then declassify-but-ITAR the good stuff, and then you can just use commercial transport services. Half the reason we have to be careful with advanced tech as a nation is because those yellow weasels will steal anything that isn't nailed down.

>> No.11491391

>>11490872
https://www.youtube.com/watch?v=4hZ5Ep06TTk

>> No.11491531

>>11491352
That's the same reason we don't let them dock on the ISS.

>> No.11491565
File: 8 KB, 367x241, 40199AAF-FE7A-445F-9960-643D505F6E4B.jpg [View same] [iqdb] [saucenao] [google]
11491565

>>11491322
Because its the most reliable rocket in service.

>> No.11491574

>>11491565
>Because its the most reliable rocket in service.
JWST was designed for Ariane 5; back in 1996, there were limited options for beyond-LEO launch vehicles with significant payload capabilities. In 2003, when the actual contract for building it was awarded, neither Delta IV nor Atlas V had proven themselves as reliable launch vehicles. Ariane 5 was the only vehicle that fit the bill.

>> No.11491584

>>11491106
But everyone who is going to space does speak Russian already. Learning it a part of the training. LK is not Soyuz, and the Moon landing was just a propaganda mission and a dead end which led the humanity nowhere. The original Venus flyby and "slow and steady exploration" concept was miles better.
>also wed have reusable energia boosters by now
Energia was built by Glushko, not Korolev.
Korolev wasn't some kind of ancient soviet spaceflight god, he had his share of mistakes, notably bying the Shukhov's hyperboloid meme with N-1 which turned out not to be as light as he hoped, and using it instead of just scaling the perfectly fine R-7 parallel layout he already had working, which could have been tested on a much smaller/cheaper stand. There were dozens of better engineers with better vision in the union. Mishin was a terrible lead, but that's just him.
>the buran was notably superior to the shuttle
it was the same useless contraption, and automation was a meme to start with

>> No.11491586

>>11491565
Probably not the most, but actually quite reliable

>> No.11491702

>>11490872
I still mourn this glorious meme machine.

>> No.11491720

>>11491391
If only soviets hadn‘t used some fucking pinhole camera to document these.
Also I‘m not sure the explosion effects used in here are accurately large.

>> No.11491843

>>11490678
jfc, bezos is one of the richest people in the world and has the audacity to do that? just pay out of your own pocket you greedy bastard

>> No.11491884

>>11491843
That's fucking pennies compared to what Boing seems to be wanting. $150bn, son.

>> No.11491899
File: 40 KB, 340x311, gals-small.gif [View same] [iqdb] [saucenao] [google]
11491899

Damn the Jovian quartet is so shmecksy. I call dibs on Ganymede. Going to drill a base in her crust.

>> No.11491930

>>11491320
No, they're just going to stuff it in the cargo hold of Starship because it had its first launch 5 years earlier, three of those years were the time it took to decide to do that, and two more lightning fast years to figure out how to put it in.

>> No.11491934

>>11491884
sad thing is they'll probably get it

>> No.11491939

>>11491934
Oh yes.

>> No.11492037

>>11491930
contracts are already signed, anon

>> No.11492040
File: 105 KB, 850x478, 1533c586c92af680ddd330cff927c516.jpg [View same] [iqdb] [saucenao] [google]
11492040

>>11491574
>2003
how the fuck does the USGov expect to get anything done with their souls weighed down by gravity like that

>> No.11492062

>>11492040
T. Pedo who got erased from space-time

>> No.11492076

>>11490883
Kek, its like watching Donald's response going from "its not a problem, fake news" to "shut it down!"

>> No.11492078

>>11491132
Heh, you must be new around here

>> No.11492079

>>11491301
>2030
wooow bucko, slow down. whats up with the unrealistic date, its way to soon

>> No.11492091
File: 86 KB, 337x441, 15812498274420.png [View same] [iqdb] [saucenao] [google]
11492091

>>11490883
>listening to experts in every matter
>ever

>> No.11492106

>>11491884
>>11491934
>>11491939
Boeing actually want $60 billion for the commercial aerospace industry, not just them. That sum is getting splitting up between a lot of different companies, though Boeing will likely take a big chunk of it because their the lynchpin holding up the US commercial aerospace industry.

>> No.11492110

>>11492106
more like, holding back the US commercial aerospace industry

>> No.11492137

>>11490678
For some reason, I had mixed Jeff Bezos with John Bigelow and was excited Elon was gonna collab with him and build that starship warship i kept sperging about. Oh, and I made a space roleplay here lmao have fun
https://www.roblox.com/games/4796904739/Mars-2045-Sci-Fi-RP

>> No.11492146

>>11491323
I've heard of elon sperging over the legs being too small. Maybe they're just waiting for preassembled bigger landing legs

>> No.11492151

>>11490883
Disingenuous. There's 8 billion people. 200K/8 billion is literally nothingburger. 50 million people get sick with flu each year.

>> No.11492152

>>11492137
your soul is weighed down by gravity

>> No.11492161

>>11492152
>your soul is weighed down by gravity
Ain't that the fucking truth.

>> No.11492303

>>11491899
Ganymede is named after a male child lover of Zeus, you pedofag

>> No.11492317

>>11491391
Why did it keep failing!!!!!!

>> No.11492322

>>11492317
Korolev died

>> No.11492625
File: 370 KB, 1798x1024, EC49E948-DC79-43DC-B8E6-B1201E983AB7.jpg [View same] [iqdb] [saucenao] [google]
11492625

https://youtube.com/watch?v=ucJCeT7l2cc&feature=emb_title

Coming soon...

>> No.11492798

>>11492303
OH SHIT I'LL TAKE CALLISTO I'LL TAKE CALLISTO! Well at least she doesn't experience so many sieverts, perhaps that's a better destination anyways.

>> No.11493000

>>11492625
At least they're making progress despite corona. Hope the craft works well for them. Maybe it'll put some pressure on NASA to make them work faster.

>> No.11493023
File: 157 KB, 676x454, JackParsons3.jpg [View same] [iqdb] [saucenao] [google]
11493023

why did the government kill him, anons!?

>> No.11493026

>>11493000
>Maybe it'll put some pressure on NASA to make them work faster.

NASA can’t really work at all in the current situation...

>> No.11493033
File: 537 KB, 500x257, ACA4101A-9489-44DD-BFE6-7D49C8DCB8D1.gif [View same] [iqdb] [saucenao] [google]
11493033

https://www.thetalkoftitusville.com/post/ksc-worker-confirmed-with-covid-19

>> No.11493043
File: 7 KB, 225x224, so_it_begins.jpg [View same] [iqdb] [saucenao] [google]
11493043

>>11493026
I meant outside of the breakout freakout.

>>11493033
>mrw

>> No.11493079

>>11493033
I thought it was already closed.

>> No.11493604
File: 88 KB, 750x420, pfrc-2-pulse_feature.jpg [View same] [iqdb] [saucenao] [google]
11493604

Anyone know much about this thing? Is it/ the people working on it legit? Think it has a chance of working? I don't know too much about fusion other than it's taking a while.

https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20170003126.pdf

https://en.wikipedia.org/wiki/Direct_Fusion_Drive

>> No.11493607

Time to shut these threads down for a month
Othing is happening

>>11493604
Fusion anything is not real

>> No.11493609

>>11492322
Damn, Korolev seems to be the big brain in the Soviet Space program. But how isn't he listed as the most important?

>> No.11493617

>>11493609
he was the director/leader of the soviet space program until his death
he was less of a technical genius like Werner von Braun and more of a political genius
without his connections and allies the Soviet bureaucracy was incapable of getting anything done

>> No.11493618
File: 19 KB, 584x233, moonbase.png [View same] [iqdb] [saucenao] [google]
11493618

https://twitter.com/DEFCONWSALERTS/status/1241896753483272192?s=20

Anything to this? Just a rumor?

>> No.11493642

>>11493618
big if true

>> No.11493647

>>11493618
t. Two countries that are lacking rockets to do anything past LEO

>> No.11493658
File: 8 KB, 277x271, proofs.png [View same] [iqdb] [saucenao] [google]
11493658

>>11493618

>> No.11493670
File: 749 KB, 840x615, 20131223_yutu_f840.png [View same] [iqdb] [saucenao] [google]
11493670

>>11493647
Anon, China sent rovers to the moon already, what do you mean they lack rockets to get beyond LEO? Not sure on Russia though.

>> No.11493678
File: 314 KB, 2000x1125, falconheavy.jpg [View same] [iqdb] [saucenao] [google]
11493678

>>11489725
they put plastic down for the crane my god! Not going to make it.

>> No.11493687

>>11490206
to bad they are not bringing back a centaur

>> No.11493690

>>11493670
>1200 kg lander

Apollo was 5000kg
Modern landers will be heavier

>> No.11493699

>>11493690
That doesn't mean China "lacks a rocket to do anything past LEO" but I agree with your semi-related point about them needing bigger landers if they want to bring stuff larger than a desk up there.

>> No.11493700

>>11493618
Russia’s Moon plans are in a permanent state of limbo, so I wouldn’t read too much into anything unless an agreement is signed or joint program started.

>> No.11493709

>>11493699
Bigger lander needs bigger rocket, much bigger

>> No.11493710

>>11493700
>”We’ll contribute to the Gateway, it’ll be like an ISS but around the Moon! Actually...we’ll build our own space station at the Moon out of un-launched ISS modules that are lying around because Russia stronk!...Oopsie, we can’t actually afford that, so we’ll just partner up with our new buddy China!”

>> No.11493713

>>11493690
Stop bringing Apollo. It was a single-launch mission to nowhere. Nobody is going to do single launch missions anymore for this, neither NASA nor SpaceX not anyone else. You land at least hundreds of tons of equipment, if you are going to do at least something useful and not just plant a flag, no single rocket is going to do this.

>>11493647
>>11493618
Technically both plan superheavy rockets, but lack the capability.

>> No.11493723

>>11493647
>>11493699
This >>11492625 will raise it’s orbit to 8,000km (MEO) for a high-speed re-entry test after it’s April launch on a LM-5B. So technically, the Chinese do have a crew capsule able to travel beyond LEO...

>> No.11493726

>>11493709
Not really. You just assemble it in orbit from smaller pieces and deliver fuel separately if needed. It's not 1968 anymore. With reusable rockets it will be even cheaper than with an expendable large one like SLS.

>> No.11493731

>>11493723
Oh neat, I had wondered what that was for.

>> No.11493734

>>11493713
>>11493726
No one has done an “assemble in orbit for BEO” mission
It’s not just going to suddenly happen ether

>> No.11493736

>>11493618
I don't expect much from this desu. I do honestly want this to be a big deal and make good progress, but I'll only take it seriously when I see them make good progress on it.

>>11493726
B-but reusable rockets are just a meme. Blunderf00t said so!

>> No.11493740

>>11493734
No one did orbital rendezvous when the Lunar orbit rendezvous mission mode was selected for Apollo. But what was done after that was that tests were conducted to figure things out. Not just small meaningless tests for grants, actual implementation of hardware to learn something useful. If we're just going to limit our space flight missions to what has been done before, then we'll never leave this rock.

>> No.11493745
File: 10 KB, 276x183, iss.jpg [View same] [iqdb] [saucenao] [google]
11493745

>>11493734
>No one has done an “assemble in orbit for BEO” mission
And? Does it make this impossible or what? Orbital assembly is mastered long ago.

>> No.11493750
File: 354 KB, 1920x1280, milkies.jpg [View same] [iqdb] [saucenao] [google]
11493750

So given the size of starship and the supplies needed for a large crew, is physically blocking cosmic radiation viable by just having all the cargo in the exterior compartments of the ship?

How many feet deep of stuff do you need to block radiation for a year?

>> No.11493756

>>11493700
Just like American ones, oh wait

>> No.11493765

>>11493750
Why not just dedicate a Starship for interplanetary travel and build an ice shield around it Magellan-style using moon-water?

>> No.11493785

>>11493750
You can design the crew compartments to be surrounded by water and that will take care of most of the radiation.

>> No.11493794

>>11493765
Because physics?

>> No.11493885

>>11490953

I thought minimizing dry weight is everything in spaceflight? How can increasing your weight be better than a more expensive but lighter heatshield, especially for an interplanetary craft?

>> No.11493892

So what happens to those 74 OneWeb satellites currently in orbit? They're pretty much useless since the constellation is very far from completion.

>> No.11493900

>>11493885
>I thought minimizing dry weight is everything in spaceflight?
No, and that's a poor mindset to have. There's more to spacecraft design that needs to be taken into account. Especially when reuse is a part of the mission.

>How can increasing your weight be better than a more expensive but lighter heatshield, especially for an interplanetary craft?
Well first, that's a prototype so dry mass isn't a concern for now. Second, I assume you're referring to the steel construction, that material can handle extreme heat loads better than lighter materials which means a thinner heat shield can be used and that usual ways of dealing with temperatures can be discarded which saves on weight. Also, steel is much more ductile than aluminum which makes the vehicle more durable, which is needed for reuse.

>> No.11493930

>>11493900
Thinner heat shield, maybe, but the perspiration liquid cooling system they're adding/need on top of that sure to add even more weight.

>> No.11493934

>>11493930
I thought they dropped perspiration cooling for just tiles? I think it was TUFROC?

>> No.11494025

>>11493885
I have no idea what the fuck I've talking about, but the reasoning I keep hearing is that the heatshield isn't so light because the aluminum isn't robust at extreme temperatures. I believe the entire space shuttle had thermal protection whereas the intention for starship is to have about half coverage that can be thinner.

But like >>11493900 said. It's a trade off. If your rocket takes more fuel and tops out at slower speeds, but it can still do the missions you need and its reusable, you've found the winning balance.

>> No.11494029

>>11493930
>>11493934
They did drop the sweating thing

>> No.11494065

>>11493885
>How can increasing your weight
Except you're not if you account for steel being stronger than composites at cryo temps and than aluminium at high temps, for a small fraction of the price while at that

>> No.11494068

>>11489376
Question: what is the best way to bring the cost of the SLS down?

>> No.11494081

>>11494068
Build them outside so they keep getting destroyed.

>> No.11494088

>>11493750
>How many feet deep of stuff do you need to block radiation
For cosmic rays, you need to be surrounded by a shell of water ten meters thick to provide equivalent shielding as exists on the Earth's surface. Nothing else works, magnetic fields in particular only divert solar wind and do FUCK ALL to block cosmic rays, the particles are simply too high energy. Mass mass mass is what you need for your ass. Of course, bringing field levels down to ambient on Earth's surface is overkill, you only need a fraction of that (but still several meters worth) to fit inside the maximum annual dose limits for nuclear energy workers, which would actually mean that those astronauts would be getting less dose than people currently do on the ISS.

>> No.11494094

>>11493892
Scrap em, deorbit, they're junk, waste of parts

>> No.11494100

>>11494068
Centralize manufacturing of all components within a single state.

>> No.11494112

>>11494068
Really isn't any way at this point other then what this anon pointed out
>>11494100
Reusable rockets are the future.

>> No.11494119

>>11494112
>Reusable rockets are the future.
Yeah I think so too, if NASA got behind it and manufactured all the components in a single state or even a single facility, the cost savings would be enormous. Splitting something up between 50 states just so everyone votes on it is fucking gay, stop it.

>> No.11494123

>>11494119
I believe the main reason why they can't do this is they would need congressional approval. That's why NASA seems so slow compared to private space companies.

>> No.11494138

>>11493930
>Thinner heat shield
Thinner on the belly, absent entirely on the backside.
Mass per square meter of the finished vehicle is structure plus TPS. If they did carbon composites, the TPS needs to be waaaay thicker and cover twice as much surface area. The carbon composite structure is also only marginally lighter than aluminum at best because of the amount of additional support structure needed for carbon composite joinery. With aluminum the TPS thickness is almost as bad. With steel however you eliminate half of the TPS coating entirely and the other half goes from half a foot thick to less than an inch thick, a huge reduction in mass. Also, since steel is tougher than aluminum or carbon composites and much easier to handle, you can actually go much thinner with your material and end up with a finished stage that is lighter than anything that can practically be built at that scale using aluminum alloys or CC (this is why Centaur uses steel tanks and gets the most delta V of any upper stage vehicle and why in the 50's we were capable of manufacturing balloon tanks out of steel for the Atlas that let it achieve almost SSTO performance).

All of the highest mass fraction rocket vehicles in history have been made of steel. It's more incredible that nobody really connected the dots like this before and realized they could ditch aluminum and other meme materials for good old steel and get the same or even better performance in many cases.

>> No.11494143

>>11494123
Of course, it's like asking them to vote on tighter term limits for themselves, no way they say yes.

>> No.11494148

>>11493885
>I thought minimizing dry weight is everything in spaceflight?
It was early on, till early 80s or so. Ease of manufacturing, cost, and many other factors are also taken into account since then.

>> No.11494292

question: all explanations for the use of stainless steel over aluminum make aluminum sound literally retarded. Why did it become standard practice in the first place?

>> No.11494436

>>11494292
It's actually quite decent if you don't care for reentry or reuse. Also muh space age material. It can't handle high heat and develops fatigue cracks easily, but it's not a problem if you throw it away upon reaching orbit, and your only major headache left would be welding it.

>> No.11494446

>>11493618
Load of bullshit.
China wants nothing from russia.

>> No.11494449

>>11490872
>>11491391
Were any of the N1 launches manned? So little info from the cold war.

>> No.11494466

>>11494449
No, and it's highly unlikely that they lied about that. Not even the Soviets were insane enough to put crew on a new rocket with zero successful launches.

>> No.11494482

>>11494449
Of course. Every stage was manned by an expendable gulag prisoner.

>> No.11494488
File: 70 KB, 379x452, ea55IwCXBXY.jpg [View same] [iqdb] [saucenao] [google]
11494488

>>11494466
>"even"

>>11494449
Cold war is not the problem, your laziness is. There's plenty of info about N-1 and the soviet program.

>> No.11494498
File: 864 KB, 2048x1415, 1553996535787.jpg [View same] [iqdb] [saucenao] [google]
11494498

>advanced, rich country
>lots of people
>scifi media is popular
why isnt spaceflight bigger in japan?

>> No.11494512
File: 65 KB, 1024x724, 2cfb8b6a10b9d869efc4ee05cbd2dae0.jpg [View same] [iqdb] [saucenao] [google]
11494512

>>11494498
It's fairly big, they just don't have a manned part. Their program is a legitimate science/high tech driver in the country, not just a job generator or a national pride thing. They do extremely well in spacecraft engineering. I'd say this is one of the most pragmatic space programs ever.

>> No.11494522
File: 154 KB, 1200x800, jaxa-hayabusa-2-ryugu-landing-artists-conception.jpg [View same] [iqdb] [saucenao] [google]
11494522

>>11494512
The Hayabusa2 asteroid sample return mission is a good example

>> No.11494547

>>11494522
Yeah. Also their LH cryocoolers with neon ice tanks are literally black magic. Pity they lost Hitomi to such a basic mistake. Had it worked, it would have surveyed the sky in >10keV before the Spektr-RG (which has been planned since forever but it's Russia so they didn't have money, only launching it recently)

>> No.11494554

>>11494547
>LH
LHe

>> No.11494555

>>11494498
They have the largest module on the ISS and an active space program. As small but powerful island nations go they’re lapping the UK.

>> No.11494597

>>11493734
we've attempted multiple "assemble in orbit" missions and one successful "assemble in LEO to travel beyond LEO" mission
that's like half the purpose of the Gemini program

>> No.11494613

>>11493934
Elon's talking about using some sort of positive pressure transpiration to seal the joints, which sounds like a good idea to me

>> No.11494634

>>11494449
No, it was all dummy payloads. Some of those were actually saved by successful launch abort systems. So even if you entertain the idea that they had put people on it, they would‘ve been fine anyway.

>> No.11494660

>>11493734
>No one has done an “assemble in orbit for BEO” mission

All of the Apollo missions were assembled in orbit, dummy. The lunar module is packed under the command module in the fairing and then flies around to the front of the command module to dock there before heading to the moon.

>> No.11494684

>>11494660
Other way around. Apollo missions did their burn into lunar insertion, then did the separation and reassembly while underway.

>> No.11494694

>>11494660
wait, so how was the CSM and S-IVB and LEM packed up in there
it was S-IVB on the bottom making the entire TLI burn, then the fairing with the LEM in it, and then the CSM on top of that?

>> No.11494698
File: 123 KB, 1143x1395, Saturn_v_schematic.jpg [View same] [iqdb] [saucenao] [google]
11494698

>>11494694
First & Second stage to get you off the rock and into orbit. Third stage for lunar insertion. Under third stage sat the LM, on top of the LM was the CM.

>> No.11494702

>>11494698
the S-IVB completed both TLI and parking orbit insertion, the S-IC and S-II didn't have enough ISP to get the whole lunar stack to orbit

>> No.11494716

>>11494694
>it was S-IVB on the bottom making the entire TLI burn, then the fairing with the LEM in it, and then the CSM on top of that?

Yes. I was a bit wrong, as >>11494684 pointed out.

After the TLI burn was performed, the command module separated from the Saturn V’s upper stage , turned around, and docked to the lunar module, then pulled the lunar module away from the Saturn V’s upper stage. The capture burn is performed by the service module’s engine and the Saturn V’s upper stage simply smashes into the moon or flies off into an orbit of the sun, where they become curiosities to be rediscovered. https://en.m.wikipedia.org/wiki/J002E3

>> No.11494720

>>11494702
>the S-IVB completed both TLI and parking orbit insertion

No, the Apollo missions performed their capture burn using the service module, and also used the service module’s engine to perform corrections. They disconnected from the Saturn V’s upper stage shortly after the TLI and there’s no way to stick it back together.

>> No.11494728

>>11494720
LEO parking orbit, anon, not LLO parking orbit

>> No.11494732

why have I never heard anybody proposing to go visit 2010 TK7 in the SEL-4 point?

>> No.11494742

>>11494728
Oh, okay. Sorry.

>> No.11494744

>>11494732
Eccentric orbit?

>> No.11494747

>>11494732
You’d need very high delta/v because it’s got a weird inclination

>> No.11494748

>>11494742
if the S-II had been capable of putting itself into orbit with payload, they could have ditched the S-IVB for the S-IV with the RL-10s and thrown way more mass to the moon
>>11494744
Earth's only (known) Trojan asteroid at the sun earth lagrange point 4

>> No.11494751

>>11494747
oh does it, that sucks
I'm sure there's got to be an efficient trajectory

>> No.11494756

>>11494748
Well, the reason nobody is suggesting it is A) limited budgets. B) what's the fucking point? It's a rock, there's no shortage of those flying around.

>> No.11494758

>>11494756
Rocks are cool

>> No.11494759

>>11494756
>it's a rock, there's no shortage of those flying around
it's a very close rock to Earth, in an interesting location, and we've only ever been to like, two rocks ever total tops

>> No.11494764

>>11494759
Well, if you're footing the bill I'm sure they'll get right on it. Truth is space exploration of any kind is being given less than crumbs.

>> No.11494795

>>11494512
>they just don't have a manned part
U wot m8? They're literally the 3rd country with the most astronauts

>> No.11494801

>>11494795
they don't have their own manned capsule, they put their astronauts up on NASA boats during the shuttle era

>> No.11494843

>go outside at night
>see bunch of starlink satellites doing acrobatic motions
>be amazed
>wake up and realize its all a dream
Not mad at all, even if dream.

>> No.11494861

>>11494843
I had a weird dream about trying to show my parents Starlink once
it kept moving too fast so whenever I pointed it out they'd miss it

>> No.11494884

>>11494843
I had a dream not long ago where among other things in the sky there were two satellites circling around the third one in the center. I immediately wondered if those were tethered starships. The Moon in that dream also had a small ring for some reason.

>> No.11495115

HULLO
https://youtu.be/PVO8nvb1o2w

>> No.11495117

>>11489376
I'm not doing those rockets. I'm not even with the shape of this Earth or these people. If I was in charge we'd be doing Star Trek material. Though more similar to Mass Effect. I'd take your DNA samples and data, store them so I can recreate you later which wouldn't be difficult at all. THen go out with a giant city to state size hydron collider.

>> No.11495188

>>11491301

JWST has the biggest short of discovering habitable worlds within our local area. I'd rather it not. Also, it's Hubble's successor. So also for that. Many of JWST's delays are a result of technologies that needed to be developed, built, and matured before they could be integrated into the observatory.

The delays weren't unwarranted. They weren't SLS delays where most of the tech already existed, but the cost plus contract basically meant that Boeing could play with its dick for years and not deliver while still extracting payments.

>> No.11495223

>>11495188
>it's Hubble's successor
Not arguing with the rest, but this is a meme. JWST is a specialized NIR telescope; HST sucks for NIR due to being optimized for visible spectrum and versatility. JWST is propellant-limited as L2 is not stable; HST turns 30 soon.

>> No.11495226

>>11495223
what are they using for JWST propulsion?

>> No.11495235

>>11495223

Yes, I know that JWST is a specialized NIR. But the massively increased mirror space is very helpful in gathering a staggering amount of light. Over the last 30 years, also, tech has advanced to determine what an object looks like across other EMR spectrum wavelengths based on IR or UV data.

Additionally, the success of JWST will drive future development of actual true color capture observatories that will truly succeed Hubble. It's a powerful stepping stone, and thereby a successor.

>> No.11495240

>>11495226
MMH thrusters

>> No.11495243

>>11495240
damn, that seems like a mistake

>> No.11495251

https://www.youtube.com/watch?v=Iwn4LVVvAUQ
Super Heavy will have twice the thrust of this beast.
God I can't fucking wait. Wish I could've seen a Saturn V launch in person.

>> No.11495254

>>11495188
>"cost plus contract basically meant that Boeing could play with its dick for years and not deliver while still extracting payments."
>yeah, I could finish that rocket, but I just found a 7TB zip file of SLS-kun hentai and I need to bust a nut to every image there. yes, this will have to be billed under the contract. sorry, but it's company policy.

>> No.11495255

>>11495243
There might be not enough power for SEP, and the spacecraft is complex enough already.

>> No.11495262

>>11495254

Multiply that by a 100,000 people and yeah, that's about right. Since part of the reason why it costs so much is because the rocket is built across nearly 50 states, then shipped to be assembled and tested preliminary in Texas, then shipped to Florida for actual test maiden flights.

>> No.11495263

>>11490097
essential industry
they deliver cargo to ISS
they'll be fine
Boing is superfucked tho

>> No.11495265
File: 56 KB, 769x457, 1.png [View same] [iqdb] [saucenao] [google]
11495265

RIP OneWeb

>> No.11495276

>>11495255
SEP simplifies handling and is no more complicated than fucking hydrazine plumbing
good point about the power supply

>> No.11495277

>>11495265
if OneWeb just dissolves, what happens to their existing constellation? Does it have the capability to deorbit itself?

>> No.11495281

>>11495277

It stays up there forever, until we have a Planetes style cleanup industry that will deorbit the hardware.

>> No.11495287

>>11495277
The satellites will probably be sold to someone else, and they'll repurpose the sats for something else.

>> No.11495305

>>11495277
Maybe some company other will buy it. Maybe Telesat.

>> No.11495324

>>11495240
MMH for momentum unloading, UDMH+NT for stationkeeping

>> No.11495406

>>11495324
why the fuck are those two different systems
they've got deep cryo behind the sun shield, they could keep liquid hydrogen indefinitely if they wanted

>> No.11495414

>>11495406
>why the fuck are those two different systems
Because making something simpler is just acceptable in space flight. Complexity and high cost is the way to go. In fact, if you try to send a simple dirt-cheap telescope into space, then the spirit of von Braun himself would strike down the rocket carrying the telescope and you for daring to offend space.

>> No.11495415

>>11495414
>is just unacceptable
Fixed

>> No.11495432

>>11495414
>>11495415
Werner quit when he saw the path of excess that NASA was taking

>> No.11495434
File: 2.76 MB, 2806x1321, Nerva_-_nuclear_rocket_engine.jpg [View same] [iqdb] [saucenao] [google]
11495434

>>11490498
So there's a chance we'll actually see something like this in action? Sweet

>> No.11495436

>>11495265
Bezos should offer 10 cents on the dollar. OneWeb's spectrum rights alone should be worth that.

>> No.11495450

https://www.space.com/coronavirus-lessons-for-mars-sample-return-worries.html

PP all of a sudden worth considering now?

>> No.11495467

>>11495450
it's a good thing there's no life on Mars
swear to god people need to get the fuck over cross contamination shit. Bringing a rock back from Mars is not dangerous by any stretch of the imagination and any "martian plague" is pure scifi.

>> No.11495474

>>11495467
>>it's a good thing there's no life on Mars

Pack it up boys, anon has found the answer, no need to send any more rovers or landers. Lets just cancel Perseverance now and scrap it for parts.

>> No.11495479

>>11495474
Correct rovers and landers are funding pointless and they should be doing real resource prospecting in preparations for an actual base

>> No.11495481

>>11495474
No, we get perseverance and let /g/ give it better hardware lmao

>> No.11495484

>>11495467
>it's a good thing there's no life on Mars

Prove it.

>> No.11495555

>>11495481
>/g/
Holy shit, it wouldn't reach escape velocity just from all the stickers, not to mention the meme shit like Stax headphones.

>> No.11495570

>>11495484
the galaxy is going to turn out to be very sad and empty

>> No.11495580

>>11494446
>from
They don't want to give, they're perfectly fine with taking.

>> No.11495593 [DELETED] 
File: 5 KB, 362x150, file.png [View same] [iqdb] [saucenao] [google]
11495593

so I fatfinger ONE (1) mutagen and suddenly I'm getting alpha dreams
great

>> No.11495597

>>11490304
ain't no way it has the delta-v for a 5 day brachistochrone to mars.

>Specific impulse: 47,000+ seconds

0.0

>70Mw / 60 newtons.

._.

>> No.11495607

>>11495597
>60 fucking newtons of force
it's the world's most powerful fart

>> No.11495622

>>11493607
>Fusion anything is not real

but the sun is a fusion.

>> No.11495632

>>11495607
naw, 60 newtons ain't nothing to sneeze at.

It can accelerate a kg to 10 meters per second.

space ships are bigger than that, though, so.... it's better than an Ion engine.... unless it's a nuclear powered ion engine.

;)

>> No.11495636
File: 542 KB, 2048x1536, 57EB2480-0AA2-49BB-BE96-3C80A1156ED8.jpg [View same] [iqdb] [saucenao] [google]
11495636

>> No.11495641
File: 1.31 MB, 1186x890, trapped_spung.png [View same] [iqdb] [saucenao] [google]
11495641

>>11495636
>Patrick! You gotta help me! NASA has kidnapped me, and I don't know where they're taking me.

>> No.11495644

I think it's more likely we'll live in Space Colonies rather than finding a suitable planet.

>> No.11495652
File: 129 KB, 1280x720, Aerospacelines.jpg [View same] [iqdb] [saucenao] [google]
11495652

>>11495636
>the guppy is still flying
Beautiful.

>> No.11495653
File: 817 KB, 3000x1538, 1582941155487.jpg [View same] [iqdb] [saucenao] [google]
11495653

>>11495644
Regardless of which happens we need to get out there.

>> No.11495659

>>11495644
Modified

Stanford

Torus

dude, trust me.

>> No.11495666

Dude, I think we can build a colony ship.

>> No.11495669

>>11495666
fucking captcha.

>> No.11495672

>>11495659
>>11495666
>>11495669
it appears you've made a mistake in your post etcetera
this is the last reply you're going to get

>> No.11495681

>>11495672
>this is the last reply you're going to get

wrong.

>Fractional gravity cargo rings.

>> No.11495685

>>11495681
fractional gravity radiator/solar thermal collector pairs.

>> No.11495687

>>11495659
>>11495666
>>11495669
>>11495681
I don't want to alarm you, but it appears that some total faggot gave you a tripcode without you knowing it. It's okay, there's still time to delete it, just be more observant next time.

>> No.11495696

>>11495685
Cyclotron

RCS

>> No.11495700

>>11495687
>without you knowing it
Then why was it already in my filters?

>> No.11495707

>>11495687
>but it appears that some total faggot gave you a tripcode without you knowing it.

I actually got this tripcode by accident.

I took it as "the will of the force", and decided to keep using it.

>ISP calculated by gamma.

>selective captcha harassment

>> No.11495708

>>11494751
Efficiency won't reduce minimum delta V, it just reduces wasted delta V.

>> No.11495710

>>11495555
Fucking kek'd, nice digits

>> No.11495719

>>>11495687
>but it appears that some total faggot gave you a tripcode without you knowing it.

I actually got this tripcode by accident.

I took it as "the will of the force", and decided to keep using it.

>ISP calculated by gamma.

>selective captcha harassment

Nuclear powered bussard ramjet.

>> No.11495722
File: 113 KB, 500x520, ill-just-warn-you-nows-dont-know-how-to-use-58284614.png [View same] [iqdb] [saucenao] [google]
11495722

>>11495719
forgot pic, pic related.

>> No.11495748

how's the SN3 stacking going?

>> No.11495755

>>11495719
>Nuclear powered bussard ramjet.

just ever so slightly modified stanford torus.

It was eventually meant to be a cruise liner between earth an mars.

bitches.

>> No.11495774

>>11495755
ISP
measured
by
GAMMA

>> No.11495780
File: 9 KB, 270x186, yes.jpg [View same] [iqdb] [saucenao] [google]
11495780

>>11495774

>> No.11495787

>>11495780
>>11495774
>>11495755
>>11495722
>>11495719
>>11495707
>>11495696
>>11495685
>>11495681
>>11495669
>>11495666
>>11495659
>>11495632
hey could you go away?
you're being a bother, and contributing nothing.

>> No.11495789

>>11495787
just report him for spamming and then filter him

>> No.11495800

>>11495787
>you're being a bother, and contributing nothing.

>contributing nothing.

>ISP gauged by GAMMA

are you fucking retarded?

>> No.11495803

>>11495789
This

>> No.11495805

>>11495787
>Exhaust velocity = large percentage of lightspeed.

>Gamma induced increase in mass or propellant occurs due to increased velocity.

Du yu even rocket equation?

>> No.11495809

>>11495805
*of

>> No.11495817 [DELETED] 
File: 7 KB, 225x225, wait.jpg [View same] [iqdb] [saucenao] [google]
11495817

>>11495789

>> No.11495820
File: 675 KB, 4096x795, Sea_Dragon_Stage_I_Propulsion_System_Layout.jpg [View same] [iqdb] [saucenao] [google]
11495820

>>11494292
The biggest issue with steel is that it's dense compared to aluminum. Aluminum is super lightweight, it almost unreal. The difference in densities become much more apparent for "smaller rockets" which makes ones using steel very heavy unless they use balloon tanks. Steel only pulls out ahead of aluminum for very large rockets like Starship or Sea Dragon.

>> No.11495829

What the fuck is going on here

>> No.11495849

>>11495829
beryllium combustion chambers, I believe.

>> No.11495851

>>11490752
the whitest elephant

>> No.11495857

>>11495820
or if you're going to be going through reentry heating

>> No.11495860

>>11493023
his faggot-ass Great Work killed him
wanted to be an alchemist, become enlightened
gg, Jack. shoulda kept better company

>> No.11495863

>>11493604
yes it's real
it's also pretty meh

>> No.11495889

>>11495434
BWXT is more like a modern version of Timberwind than NERVA, as it's built to be light with a relatively high TWR for a nuclear rocket.

>> No.11495932

>>11495820
Also easier to work with aluminum because it’s softer

>> No.11495944

>>11495849
Ahh I see

>> No.11495958

>>11495932
>because it’s softer
Well, that would depend on the alloy really. Nobody really uses raw aluminium for the most, especially not in aerospace or any other form of construction. The only time the company I worked for ever used raw aluminium that wasn't some form of alloy, was to make some monster 4 ton+ power switches for an aluminium melting plant.

80% of the work that company did was aluminium. Aluminium can be very many things depending on what you mix it with, that's what so nice about it.

>> No.11495964
File: 151 KB, 1125x1021, B683E717-9B09-4C73-A3DA-180577CFAD6C.jpg [View same] [iqdb] [saucenao] [google]
11495964

OK...WAIT FOR IT...WAIT FOR IT...HERE IT COMES...ONONONONONONONONONONO...LOOK AT THIS DUDE...WAIT TILL YOU SEE IT...AHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHA...LOOK AT THE TOP OF HIS HEAD!!!!!!!!!

>> No.11495970
File: 3.62 MB, 390x276, 555EF48A-A402-4ED2-9925-553A2C582ADC.gif [View same] [iqdb] [saucenao] [google]
11495970

>>11495964

>> No.11495973

>>11495964
What sources? An anonymous edit on wikipedia a little while ago that changed "is" to "was"?

>> No.11495977

>>11494498
>>11494555
also they're going to work with the US Space Force in the future according to both governments

>> No.11495980

>>11495964
OH NONONONONO

>> No.11495983
File: 869 KB, 280x158, 99341405-A1D1-472D-BBEB-762AF6DCE3D1.gif [View same] [iqdb] [saucenao] [google]
11495983

>>11495964
BIGELOW IS DEAD

>> No.11495987

>>11494138
>All of the highest mass fraction rocket vehicles in history have been made of steel. It's more incredible that nobody really connected the dots like this before and realized they could ditch aluminum and other meme materials for good old steel and get the same or even better performance in many cases.
God bless Elon.

>> No.11495988

>>11491899
How long till we take these marbles?

>> No.11495989
File: 2.37 MB, 480x204, 2C163377-6D13-4E38-9A34-3207A3A773F0.gif [View same] [iqdb] [saucenao] [google]
11495989

>>11495964

>> No.11496000

Don't ejaculate too hard over Bigelow. For all you know, his "source" is that one anonymous dude who may well just be shitposting on wikipedia.

>> No.11496004

>>11495988
Depends on how fast we get fusion engines working. Those z-pinch stabilized flow drives could get us there in under a month.

>> No.11496009

>>11496000
Multiple people have mentioned it, including Jeff Foust (a trustworthy source).

>> No.11496016

Big elbow was obviously a dead end
Spacex is not going to use any of their hardware which will be just as overpriced as any NASA “man rated” hardware
And no other company has any use for space stations

>> No.11496033
File: 265 KB, 1125x1414, 4DC51605-B5FC-444C-B872-BEA295338B97.jpg [View same] [iqdb] [saucenao] [google]
11496033

The problem here is that to comply with these regulations, most companies are just furloughing their employees and putting them on leave, not firing them all...

>> No.11496035
File: 250 KB, 1125x1387, DA19A9B1-1F9A-4362-A027-2EEFD6362BB2.jpg [View same] [iqdb] [saucenao] [google]
11496035

>>11496033

>> No.11496036

>>11495964
Man this is shitty, no specific love for Bigelow but their habs seemed by a stretch the furthest along in development. Don't know why any of these tards are celebrating as if losing one of maybe two up and coming expando-hab makers is somehow a good thing. You faggots want space missions to have to pay a billion a pop for aluminum cans forever?

>> No.11496056

>>11496033
Bigelow was still around? First news from them in a long time. Put the cart (space station) before the horse (orbital tourism).

>> No.11496060

>>11496056
>Bigelow was still around?
Bigelow has achieved more then 90% of the private space company's out there who are actually just dummy company's that funnel tax money straight in to politicians and their cronies pockets.
How many private company's do you now that have their own module on the ISS? f
Even if it's a test module, thats still huge.

>> No.11496069

>>11496060
A very successful test module no less.

>> No.11496165

>>11494292
Aluminum lets at 660C. Steel melts @ 1400C. Aluminum vehicles cant do reentry landing.

>> No.11496195

>>11495570
>the galaxy is going to turn out to be very sad and empty

Lol beta pussy. Empty space means space we can fill and make part of our GLORIOUS EMPIRE

>> No.11496198

>>11495644
Even the Moon is “suitable”.

>> No.11496276

>>11495964
The starship will allow the construction of rotating stations anyway.

>> No.11496293

>>11496016
this

>> No.11496307

>>11496036
>You faggots want space missions to have to pay a billion a pop for aluminum cans forever?
No, but billion dollar rubber inflatables are just as bad. Okay, so they can expand to three times their stowed volume, so what? They're still expensive as fuck to build.
The future is mass produced STEEL cans launched inside Starship one at a time then joined together in space, and once we have a decently sized rotating space station up, we can use it to manufacture bigger STEEL cans from 100 ton rolls of steel launched by Starships instead of relying on what can fit into a vehicle faring.

>> No.11496311

>>11496307
>Okay, so they can expand to three times their stowed volume, so what?
they're also more durable and resistant to solar wind and asteroids than steel.

>> No.11496312

a couple starships converted to space station duties will be more than sufficient for the foreseeable future. Don't even have to do a can-inside-a-can deal; why launch a space station inside of starship

>> No.11496316

>>11496198
Hell the only two worlds in the solar system that aren't "suitable" are Venus and Io. Venus is Venus, it even lures fags closer with its thin region of (((comfortable))) temperatures and pressures 50 km above hellworld, and Io has too much surface radiation and volcanic activity.

>> No.11496319

>>11496312
definitely all end-of-life starships should just be made into a giant space station.

>> No.11496324

>>11496316
Io could be mined remotely, and the same is true of Venus.

>> No.11496325

>>11496311
Nothing is durable in the face of hyper-velocity impacts, dummy. If you really really want the same or better properties than any Bigelow module, use steel with a layer of plastic on the inside and a layer of foil wiffle shield on the outside.

>> No.11496331

>>11496325
>Nothing is durable in the face of hyper-velocity impacts
Bigelow modules are basically made out of kevlar which is much MORE durable to impacts than steel. If we use steel for everything, it's for cost, not safety.

>> No.11496336

>>11496316
It'd be hilarious to see a venus colony pop and fall into hell.

>> No.11496338

>>11496336
No it’d be horrifying you psycho

>> No.11496342

>>11496336
Dirigibles don’t pop
Meanwhile your pressurized underground Martian base....

>> No.11496365

>>11496307
>we
Who the fuck is we, where's your multimillion dollar habitat manufacturing company with hundreds of employees and working prototypes, several of which are currently in orbit and/or attached to the ISS? The difference between you and Bigelow, faggot, is that up until apparently just now he was actually building habitat modules which would have radically reduced the cost and radically increased the functionality of living space in vacuum, while you and I are shitposting on a vietnamese smoke signal forum. A new steel-drum habitat manufacturer hasn't run him out of business, he didn't fold up because mass produced habs pushed him out, assuming the bad feelings of his employees are correct he's just gonna be fucking gone once the quarantine lifts, which by the way will leave Vulcan down two payloads.

>> No.11496366

>>11496324
It would be extremely hard to do either, for different reasons.
Venus has too much heat to easily work in.
Io has too much radiation, even for machines, to handle for long periods.

>> No.11496381

>>11496338
Calm down, it was a fucking joke.
>>11496342
True, but I wasn't being serious anyway.

>> No.11496466

https://kmxt.org/2020/03/anomaly-at-pacific-spaceport-complex-launch-rehearsal-no-injuries-as-a-result/

>BREAKING: “Anomaly” at Pacific Spaceport Complex launch rehearsal, no injuries as a result

>The Pacific Spaceport Complex reported an “anomaly” on a launch pad during a rocket launch dress rehearsal on Monday. The anomaly did not result in any injuries, according to Alaska Aerospace CEO Mark Lester.

>Reached shortly after the incident, Lester said “I can confirm we had an anomaly on the launch pad. We are executing our emergency checklist. We request everyone stay clear of the area to allow our crew to address the situation.”

>No details have been released yet as far as what caused the anomaly or how it may affect the upcoming launch.

>At 5 p.m. Lester said the emergency response had concluded. “The area is still hazardous and should be avoided. There will be personnel on site overnight to monitor,” he said.

>California-based rocket startup Astra had scheduled its rocket “One of Three” to launch from the Narrow Cape spaceport as early as Tuesday of this week. Astra has not yet responded to a request for comment.

Maybe Astra should focus less on moving fast and more on trying not to break stuff if they ever want to reach orbit?...

>> No.11496488

>>11496331
Hypervelocity impacts have enough energy to overcome any chemical bond. The protection you'd get from a thin sheet of lead foil positioned 10 cm from the surface of the hull would be many times more effective than a kevlar wrap with a thickness of many inches.

>> No.11496491

>>11496365
lotta words to say nothing

>> No.11496493

>>11496466
Jesus Christ lmao

>> No.11496508

>>11496466
They’ve now equalled the Falcon 1’s record of 3 launch failures in a row, but without even clearing the pad...

>> No.11496560

>>11496491
ur a faget

>> No.11496793

>>11496307
The actual future is producing steel rolls outside the Earth's gravity well from locally mined resources and using those to manufacture whatever the steel cans we want.

>> No.11496799

>>11496165
Aluminium starts to rapidly lose strength at above like 200 or 250°C. Steel does that as well, but at much higher temperature

>> No.11496824

>>11496466
Isn't the whole point to develop a fast response rocket that can be assembled and launched on relatively short notice? If they slowed down it would defeat the entire purpose of the competition they're participating in.

>> No.11496962

>>11496316
Are you forgetting Callisto?

>> No.11496965

>>11496004
noyce

>> No.11497009

>>11496824
There's also something to be said for building a functional, non-exploding rocket first and then cutting assembly time and maximizing turnaround. They already missed the competition deadline.