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

/sci/ - Science & Math


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10516182 No.10516182 [Reply] [Original]

SLS is not dead edition

>> No.10516266
File: 145 KB, 1125x1453, expendable launch vehicle.jpg [View same] [iqdb] [saucenao] [google]
10516266

This is a travesty<div class="like-perk-cnt"><marquee direction="left" width="250" height="50" behavior="alternate"><marquee direction="down" height="50" behavior="alternate">&#x26BE;</marquee></marquee></div>

>> No.10516267
File: 326 KB, 2518x1024, muskchad.png [View same] [iqdb] [saucenao] [google]
10516267

>> No.10516269

>>10516182
Previous thread

>>10509231

>> No.10516277

>>10516266
I thought the FH being able to put 60 tons into LEO was kind of a lie.

>> No.10516282

>>10516277
Can the current payload adapter/second stage even handle the weight?

>> No.10516291

For those who haven't watched it, there's a new video with Big Jim addressing space debris, Moon mission, Orion and more
https://www.youtube.com/watch?v=o2gz2E-Wrws

>> No.10516296

>>10516282
No, but only because designing it to be able to would be overkill for 99% of existing payloads, and would thus make the adapter way heavier than it'd need to be under normal circumstances. The cores can take the thrust loads.

>> No.10516297

>>10516277
It has the thrust and the delta V, what it needs is a stronger payload adapter, but that's literally just a case of thickening the metal it's made from. the reason they haven't yet is because there aren't any payloads heavy enough to justify the expense.

>> No.10516305

>>10516266
can this put Orion to lunar orbit or just a flyby

>> No.10516306

>>10516266
whats with the bouncing ball_?

>> No.10516311

>>10516306
>he hasn't a verified 4chan account<div class="like-perk-cnt"><div style="text-align:right"><img alt="" width="32" height="32" src="//s.4cdn.org/image/temp/verified.png"></div></div>

>> No.10516313

>>10516311
what a cuck. pic related<div class="like-perk-cnt"><img alt="" width="77" height="13" src="//s.4cdn.org/image/nofile.png"></div>

>> No.10516315
File: 488 KB, 960x726, 1553678087174.png [View same] [iqdb] [saucenao] [google]
10516315

>>10516311
>Paying to shitpost
Wew lad

>> No.10516329

>>10516266
It honestly doesn't look half bad, in fact I like it just for the fact that it demonstrates how don't need 'muh amazing hydrogen Isp giant tank RS-25 engines' to get a payload like Orion to the Moon, you can do it with engines literally 1/3rd less efficient and a smaller rocket overall.

Too bad this entire idea is not serious, and only meant to be a shot across the bow for the people in charge of SLS in order to try to get them to wake up and get their shit together.

>> No.10516332

>>10516305
Lunar orbit, the Falcon Heavy would drop off the Orion capsule + ICPS in low Earth orbit at the same altitude and speed that SLS would. From there the mission is identical.

>> No.10516339

>>10516332
Why not use the Dragon Crew instead?

>> No.10516344

>>10516339
dragon can't go as far as the moon right?

>> No.10516353

>>10516332
>at the same altitude and speed that SLS would
remind me why do we need SLS again?

>> No.10516355

>>10516353
>remind me why do we need SLS again?
That's the secret, Anon. There isn't anything being made that we need SLS for.

>> No.10516357

>>10516266
Ah, this is fully expendable. Now I can sort of understand. Was really confused at first.

>> No.10516362

>>10516353
But anon don't you care about muh jerbs, what if we ever need to build another 5000 ICBMS at a moment's notice?

>> No.10516364

>>10516266
L


O


N


G
B


O


I

>> No.10516365
File: 24 KB, 285x368, 1524642836097.png [View same] [iqdb] [saucenao] [google]
10516365

>>10516266
franken-rocket

>> No.10516377

>>10516266
So assuming they are not just talking out of their ass to scare NASA, how long could it take to get this ready?

>> No.10516380

>>10516377
SpaceX could have their part and the payload adaptor ready in a matter of months likely. The other parts? That's ULA and NASA time buddy, so like, years?

>> No.10516385
File: 1.90 MB, 316x213, 1406615983613.gif [View same] [iqdb] [saucenao] [google]
10516385

>>10516266
>well we could spend dozens of billions of dollars to build our own rocket over the next 5 years
>or we could just pay these guys to launch it next month

>> No.10516400

>>10516297
This is assuming that Falcon 9 specifications are correct, which they aren't. For some reason SpaceX is overstating its capabilities, or maybe giving the capabilities it can do in some perfect-condition computer simulation. In reality, F9 expendable can't do 23 tons to LEO and FH can't do 64. More realistic numbers are 19-20 for F9 and 50-55 for FH.

>> No.10516411

>>10516297
Yeah, but as far as I know one single Merlin 9 doesn't have enough thrust to push that much payload plus the fuel of the second stage. IIRC the payload restriction is something like 30 tons or so.

>> No.10516530

>>10516266
as long as it gets us to the moon I don't give a fuck. It could look like a big purple dragon dildo for all I care. Let's not forget that the SLS is basically made from shuttle parts.

>> No.10516531
File: 1.64 MB, 400x400, 1553875802596.gif [View same] [iqdb] [saucenao] [google]
10516531

BOOTS ON THE MOON 2024

>> No.10516538

>>10516531
LETS FUCKING GOOOOO

>> No.10516545

>>10516531
Finaly! Some progress! Lets hope that it doesn't get pushed back to 2042 to appease contractors.

>> No.10516549
File: 197 KB, 650x684, boot-altama-305302-men-s-vengeance-sr-8in-lightweight-side-zip-desert-tan-1.png [View same] [iqdb] [saucenao] [google]
10516549

>>10516545
It's going to be a cargo mission.
Boots, one pair, delivered!

>> No.10516568

>>10516549
In which NASA gets strong-armed by congress to contract Boeing in making a special cargo adapter for the boots. This somehow takes 3 years and $30M to develop. Each unit costs $3M and requires a specialist to attach the boots into. When literally anyone but Boeing were asked how they would do it, they just suggested using ropes.

>> No.10516612

>>10516400
Source?

>> No.10516615

>>10516400
The desire for sources intensifies

>> No.10516622
File: 1.68 MB, 1280x720, [HorribleSubs] Love Live! Sunshine!! S2 - 04 [720p].mkv_snapshot_01.44_[2017.10.29_02.52.02].png [View same] [iqdb] [saucenao] [google]
10516622

>>10516182
>Starship
>NASA going back to the Moon
>JWST
>EU Extra Large Telescope
>Chinks want moon bases
>Indians getting in the race

I want to sleep for 5 years to see what comes out of this.

>> No.10516629
File: 3.07 MB, 5067x3801, IMG_7182 (2).jpg [View same] [iqdb] [saucenao] [google]
10516629

Pics from the launch site this morning. -NSF

>> No.10516634 [DELETED] 

>>10516530

>> No.10516675

>>10516612
>>10516615
http://www.spaceflightfans.cn/wp-content/uploads/2018/12/falconusersguide2019.pdf

Now see what you CAN NOT find and ask yourself why.

Also, there was a launch last year where they first planned to do a drone ship landing and then scrapped it although the payload was so lightweight it should have left them more than enough Delta-V for a drone ship landing if those specifications were actually right; assume though they are actually a bit lower than that and you could see why they had double-thoughts about it.

>> No.10516687

>>10516675
Your conspiracy is based on this???
>>Mass-to-orbit capabilities for the Falcon 9 and Falcon Heavy fairing configuration are available upon request.

>> No.10516696

>>10516687
You left out the second part idiot.

Also yes, not giving any mass capability at all is strange.

>> No.10516704

>>10516675
>Also, there was a launch last year where they first planned to do a drone ship landing and then scrapped it although the payload was so lightweight it should have left them more than enough Delta-V for a drone ship landing if those specifications were actually right
Which launch are you talking about specifically?

>> No.10516705
File: 183 KB, 640x960, f798465498dfeFGG6879.jpg [View same] [iqdb] [saucenao] [google]
10516705

>> No.10516717

>>10516704
https://www.nasaspaceflight.com/2018/03/spacex-50-falcon-9-heavy-hispasat-launch/

>> No.10516722

>>10516717
A drone ship landing was planned, but scrapped due to unfavorable weather conditions.[270] SpaceX left the landing legs and titanium grid fins in place to prevent further delays, after previous concerns with the fairing pressurization and conflicts with the launch of GOES-S.[272]

>> No.10516732

>>10516717
Thank you.

>The company’s recovery fleet, including the drone ship Of Course I Still Love You, put to sea on 21 February to support what would, if it had been attempted, have been SpaceX’s most ambitious core recovery attempt to date.
I don't have the time right now to look into this but it seems like there were factors in that launch that made recovery difficult and not due to some limitation in the design.

>> No.10516739

>>10516717
>>As weather conditions at sea have prevented recovery operations from taking place, the core was instead disposed of into the ocean
Dont make me look at weather reports for that time.....

>> No.10516743

>>10516722
You've also got to consider this was during the phase when SpaceX were purposefully dumping Block 4 boosters.

>> No.10516765

>>10516704
I don't know, but there are many such flight. Theoretically, SpaceX should be able to land GTO missions up to ~7 tons on a drone ship, but those dont get a landing attemt at all. It should also be able to put ~5 tons into GTO and RTLS but those get landed on a drone ship. Add to this the fact the user manual is secretive about capabilities and you get the picture why a lot of people think SpaceX is overstating the capabilities of the F9.

>>10516687
You know, if they want you to just call them they could have avoided publishing a user guide altogether. Leaving out typical mass capabalities is weird as fuck, like a car manufacturer not telling you how much gas the car typically consumes.

>> No.10516792

>>10516629
This doesn't look very mobile

>> No.10516804
File: 73 KB, 1172x274, em.png [View same] [iqdb] [saucenao] [google]
10516804

ice a shit

>> No.10516811

>>10516804
>>SPACE X is DED !!!! Pack your bags and go home. The show is over

>> No.10516827

>>10516804
>not heating the valves with Boring Company TM flamethrowers
wew lad

>> No.10516830

>>10516266
Looks like it can snap in half easily.
t. layman

>> No.10516832

>>10516830
I played enough Kerbal Space Program with FAR to know that it's impossible to get that thing into orbit without doing a couple backflips on the way up.

>> No.10516835
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10516835

>>10516792

>> No.10516855
File: 368 KB, 2817x1574, Commonality_DIRECT.jpg [View same] [iqdb] [saucenao] [google]
10516855

>>10516530
>SLS is basically made from shuttle parts.
they didn't even do it the right way as intended by the engineers, NASA workers, etc who came up with DIRECT, instead they did it so SLS could become a pork barrel project sustaining jobs/elections/congressmen, etc..

>> No.10516860
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10516860

>>10516855

>> No.10516883

>>10516855
At least SLS is starting to get some real scrutiny from the government now. Hopefully it flies some real missions to the moon before other super heavy rockets fly.

>> No.10516885

>>10516860
I like to imagine the shuttle gets thrown into a waste paper basket when it goes off screen.

>> No.10516897

>>10516266
SpaceX decided not to human rate the FH.
Who's going to buy the 7 launches needed?
This is a Kerbal tier hodge podge and could destroy the rocket/take too long to adapt the SLS third stage to fit the FH

>> No.10516905

>>10516266
Falcon is too skinny. Why can't SpaceX at least make a wider core stage? A wider stage might even be easier to land.

>> No.10516911

>>10516629
Wasn't this supposed to have 3 Raptors?

>> No.10516917

>>10516911
iirc the second hopper will have 3

>> No.10516919

>>10516905
I think Falcon 9 is skinny because originally it was meant to be a smaller rocket (the Falcon 5). But then SpaceX got more funding from NASA to make a bigger launcher so they took the design they had, added more engines to the first stage, and stretched the rocket until it had the capability they needed.

As to why SpaceX isn't making a wider Falcon 9 is probably due to two things mainly. One, NASA requires a design freeze for any rocket that carries crew for them, so if SpaceX made the Faclon wider then they would have to reproof it for crew. That process takes a while. Two, SpaceX already has the production line, tooling, and expertise for the regular Falcon 9 available and it's already making them money. Changing the design to be wider would mean more expenses on SpaceX for a slightly better rocket (from their perspective at least). You can see how it's not worth it.

>> No.10516924

>>10516919
Neither of your reasons are the actual reason.

Falcon 9 is sized for road transport. It can't be made wider before it stops being legal to transport on the Interstate Highway System. A shorter, wider rocket would otherwise be preferable.

>> No.10516925

>>10516911
pretty sure they haven't even finished building the other two raptor engines. They were supposed to do various single engine tests while waiting for the other two to show up, then once those were there and bolted on it'd actually start doing the hopping.

>> No.10516948

>>10516924
I was not aware of this. Is there documentation about that?

>> No.10516991

>>10516948
have you ever seen one of them on a truck? it barely fits
other than that, no I don't have papers but that other anon might`

>> No.10517004
File: 567 KB, 3264x2448, WkGqHru.jpg [View same] [iqdb] [saucenao] [google]
10517004

>>10516948
A Falcon 9 has a diameter of 12'. The legal limit to trucking in the Eastern United States is 13' 6" for the total height of the trailer and load.

https://www.heavyhaul.net/trucking-legal-height-limits-map/

>> No.10517013

>>10516924
How would they have to transport it instead if it was wider, how do the wider rocket companies do it?

>> No.10517018

>>10517004
Thank you! Its always interesting to see the rationale behind these designs.

>> No.10517024

>>10517013
>How would they have to transport it instead if it was wider, how do the wider rocket companies do it?

Other rockets have been built on site, flown in cargo planes, or transported on barges.

>> No.10517025

>>10517013
Seaways.

>> No.10517031

>>10517024
>>10517025
why not train

>> No.10517037

>>10517031
just use a blimp train

>> No.10517039

>>10517037
what about a large cannon that fires rockets across state to their designated launchpads?

>> No.10517041

>>10516835
Oh yea? And where is the engine with all the piping that grounds this beast?

>> No.10517050

>>10517039
just fucking fill them up and fly them wherever you need them to be
the droneship landings are like 1000 km out aren't they? Plenty of distance for a core to transport itself
>>10517041
all the piping is self-contained
I haven't seen them install quick-release on the fill-hoses yet tho
it's kind of a moot point because the whole thing's tied down right now

>> No.10517051

>>10517004
Haha imagine igniting the rocket while it was on the back of the truck haha would that be cool? A rocket truck lol

>> No.10517101

>>10517004
Thanks, very interesting to see how the law limits engineering decisions in completely unrelated things, ie. rockets

>> No.10517105

>>10517051
New land speed record!

>> No.10517110

>>10517101
>Thanks, very interesting to see how the law limits engineering decisions in completely unrelated things, ie. rockets

You're welcome - although to be fair, it was SpaceX's decision to rely on the Interstate Highway System to move their rockets.

>> No.10517134

fun fact, Boeing's -900 etc fuselages are length they are because of... tunnels
if they were any longer they'd hit the inside of the train tunnels when they curve

>> No.10517143

>>10517051
this is how you build up extra horizontal velocity

>> No.10517150
File: 168 KB, 1200x800, 140706-boeing-fuselages-jms-1758_d1e183a8786b78378a2615205f45f508.nbcnews-fp-1200-800.jpg [View same] [iqdb] [saucenao] [google]
10517150

>>10517134
boeing transports fuselages by train and sometimes they get thirsty

>> No.10517198

>>10517150
those people are getting too close to those eels

>> No.10517215

>>10517198
That pic is from "Boeinssic park" trailer

>> No.10517231

>>10517150
>>10517198
Jesus Christ these MCAS accidents are getting out of hand

>> No.10517238

Two Soyuz launches on April 4. Can Russia accomplish it?

>> No.10517241

SpaceX should just start building its rockets near the place where it's going to launch them. How hard could it be?

>> No.10517249

>>10517238
Russia's only launching one Soyuz on April 4

>> No.10517256

>>10517238
Baikonur and vostochny?
Impressive...

>> No.10517258

>>10517256
Baikonur and Guiana but both rockets are Russian

>> No.10517281

>>10517150
>Ethiopian Airlines Simulator 2019

>> No.10517282

>>10516182
by travesty you mean proof of adapting, creativity, and a feat of engineering? Yes. They took a crappy situation and are open and flexible to make changes mid stride.

>> No.10517443

>>10516717
Was a block 4 booster, not block 5

>> No.10517447

https://youtu.be/hHG3Z0O9Xzo

A cool animation of Sea Dragon that I've found. Thought that you guys might like it.

>> No.10517449
File: 432 KB, 2048x1536, D3JqJyxWAAUoW56.jpg [View same] [iqdb] [saucenao] [google]
10517449

>> No.10517502

>>10517258
>Guiana
So it not Russian. Guiana operated by ESA, so it european rocket.

>> No.10517509

>>10517502
Roscosmos operates the Soyuz it sells to Arianespace

>> No.10517523

>>10517051
https://www.youtube.com/watch?v=_JENG0Z8AMk

>> No.10517531

>>10516629
Wasn't this bastard supposed to have hopped yesterday?

>> No.10517533

>>10517531
valves are freezing
t. musk

>> No.10517537

>>10517502
>european rocket
ruski rocket with commercial payload

>> No.10517541

>>10517502
I wasn't asking if Russia could handle two launches from its own territory. I was asking if these two Soyuz rockets can make it into space without any problems. Soyuz reliability is becoming very questionable. Two Soyuz launched on the same day means there is more chance for something to go wrong in that time period.

>> No.10517543

>>10516855
It occurred to me - Why not keep the exact same stack but instead of the shuttle you have an expendable faired engine, and stick the payload on the top?

>> No.10517547

>>10516860
Yeah why didn't they do this

>> No.10517550

>>10517543
Don't you mean Shuttle-C?
https://en.m.wikipedia.org/wiki/Shuttle-C

>> No.10517560

>>10517541
OK so who do you congratulate for a successful mission of Dragon2 ? SpaceX that build it or NASA that payed for the mission ?
Guess who the russians thanked.....

>> No.10517563

>>10516860
what KSP mod is this?

>> No.10517572

>>10517533
Ech, 'kin ell. My mars away bag is packed

>> No.10517586

>>10517550
Almost, but with payload on the top. Hey ho. How the fuck did NASA fuck things up so badly for so long?

>> No.10517752

>>10516400
>and 50-55 for FH.
Still good enough to launch the entire Orion + service module + ICPS into low Earth orbit as-is.

>> No.10517763

>>10516832
If your rockets are doing backflips it's because you're a faggot

>> No.10517767

>>10516905
>Why can't SpaceX at least make a wider core stage?
Tooling costs and they wouldn't be able to transport it by highway anymore.

>> No.10517777

>>10517050
usually they're only a couple hundred km out, i don't think they've ever put a drone ship out past 800 km.

>> No.10517783

>>10517447
>humans on Sea Dragon
Meh, it was nice until the animator went full retard with that staging sequence and never recovered

>> No.10517795

>>10517586
>Almost, but with payload on the top.
Because the tank wasn't originally designed to take the loads that would result from attaching dozens of tons of cargo to its nose. Any design you hear about that had the payload on the nose but didn't completely redesign the tank would have failed; that includes the Jupiter design. The only Shuttle derived vehicle that would have actually worked with zero changes to the boosters and external tank was the one where the main engines were mounted on the side as if there were a Shuttle, but instead of a shuttle there was just a big fairing mounted to the engine block.

>> No.10517799
File: 95 KB, 1068x691, D3KwHs7XsAIgljA.jpg orig.jpg [View same] [iqdb] [saucenao] [google]
10517799

thanks scott

>> No.10517814

>>10517101
this same problem affects Russian rail transport of their rockets. It is one reason nobody wants to build more Proton pads. The existing lines between the factory and Baikonur are already much wider and have more headroom than are standard.

This is also why Soyuz launches from so many places; it breaks down into many narrow parts so it is easy to transport.

>> No.10517819

>>10517777
this Falcon Heavy flight is going to have it at 967 km

>> No.10517829

>>10517819
It's also the furthest one ever

>> No.10517881

Hopper is venting again

>> No.10517882

>>10517150
They're so majestic in the wild.

>> No.10517911

>>10517829
yes, I'm sure they could launch from LA to the Cape, point to point single stage and land
>>10517881
looks like they've really got it lit up out there

>> No.10517929

QUICK

ASSUMING YOU HAD THE FUNDING TO BUILD IT, HOW FAST COULD A ROCKET MADE WITH THE PEAK OF TODAY'S TECHNOLOGY TRAVEL THE MOON? HOW FAST COULD IT TRAVEL TO MARS?

>> No.10517935

>>10517799
>Untitled Space Craft
heh

>> No.10517936
File: 161 KB, 700x436, musky boi.jpg [View same] [iqdb] [saucenao] [google]
10517936

>Despite contrary comments made one week prior, NASA administrator Jim Bridenstine has affirmed – this time in no uncertain terms – that a two-week study investigating commercial options for launching the Orion spacecraft to the Moon has concluded that Falcon Heavy could be the only practical option if NASA chooses to proceed
oh no no no no no no no

>> No.10517961

>>10517929
you could launch an impactor at the moon and it'd only take a few days to get there
>>10517936
that's the dumbest thing I've ever heard, because it's not even putting an ICPS on top of a Falcon Heavy core stage, it's putting ICPS on top of the second stage of a full Falcon Heavy stack
that's going to wiggle itself to fucking bits and look ridiculous
I hope it actually happens so we can post dumb memes

>> No.10517966

>>10517961
>wiggle itself to fucking bits and look ridiculous
then SpaceX will go
>"Unity not us :^)"

>> No.10517969

>>10517966
I hope it works desu

>> No.10517981

>>10517929
>THE MOON
three days
>MARS
six months if the planets are in the right places, right now they're pretty much as close to the worst possible alignment as you can get

>> No.10517988

>>10517961
Real life is not ksp

>> No.10518005

>Dragon 2 manned flight slipped again to October 2nd
Is there a problem that's being unreported or is it just to reduce the humiliation Boeing's under right now?

>> No.10518020

>>10517936
NASA wins either way, its the contractors who lose.

>> No.10518024

>>10518005
I'm not a huge tinfoil, but the second does seem likely.

>> No.10518040

>>10517961
So Pence says
>>"We must accelerate and accomplish this goal by any means necessary - we must focus on the mission and not the means"
So Bridenstine says:
>>it would require time [and] cost, and there is risk involved," Bridenstine said. "But guess what—if we're going to land boots on the Moon in 2024, we have time, and we have the ability to accept some risk and make some modifications. All of that is on the table. There is nothing sacred here that is off the table."
So you know what they mean by accept some risk? It means we may end up killing some astronauts before we go back to the moon. The franken rocket is sort of compelling though, ULA does do hydrogen rockets better. That's really the only good thing ULA does.

>> No.10518042

>>10518040
it's not "killing some astronauts" risk, it's "breaking a few rockets doing flight testing" risk
maybe even "welp looks like this config won't ever fly and now we're back to square one" risk

>> No.10518047

>>10517560
That's the point though. The ESA owned rocket is still a Russian rocket. If one or both of those rockets malfunction in flight tomorrow Russia will most likely get the blame. Conversely, if both make it to orbit then Russia deserves credit for the win.

>> No.10518052

>>10518042
there is nothing sacred here that is off the table.

>> No.10518056

>>10518040
Getting in your car to drive to work is a risk, grow up.

>> No.10518074

So this next Soyuz launch completes the O3b MEO constellation. I'm surprised O3b doesn't get more attention. Seems like a more cost effective way of delivering satellite broadband with much better latency than GEO comsats. Starlink and Oneweb will have even better latency of course but they need thousands of satellites to provide global coverage.
https://www.youtube.com/watch?v=ZIkpuyMgHSQ

>> No.10518075

>>10516531
>female
aaaaand it's nothing

>> No.10518079

>>10518075
First woman (male)

>> No.10518084

>>10518079
So, she won't be lonely and horny (on the moon)?

>> No.10518089

>>10517031
Rockets should be pulled by trains. It just feels so right.
https://www.youtube.com/watch?time_continue=2&v=wXRVqxJeeYw

>> No.10518126

>>10518040
>NASA should stop wasting time and money on rockets and dedicate themselves to building hardware instead
SLS cancelled, james webb accelerated, memebase alpha confirmed
god bless Pence

>> No.10518182

HOP WHEN

>> No.10518188

>>10518182
they've got methane clathrates forming in their fuel valves, so eventually

>> No.10518260
File: 1.15 MB, 500x281, 1551296924207.gif [View same] [iqdb] [saucenao] [google]
10518260

>>10518182

>> No.10518364

>>10517981
Mars is 3-5 months, not 6 months, any manned mission will be optimized for short travel time to mitigate radiation exposure.

>> No.10518369

Apparently Russia is going to launch the Progress mission first on April 4. I guess if something goes wrong with that Soyuz rocket then ESA can delay launching the next Soyuz carrying the expensive O3b satellites.

>> No.10518561
File: 137 KB, 900x597, 32582233027_90d19160e8_b.jpg [View same] [iqdb] [saucenao] [google]
10518561

It seems Starliner is experiencing more delays.

>Boeing said Tuesday the first orbital test flight of its commercial crew capsule, named the Starliner, will be delayed until August “in order to avoid unnecessary schedule pressure” and give priority on the Atlas 5 rocket’s manifest to a U.S. Air Force communications satellite.

https://spaceflightnow.com/2019/04/02/boeing-confirms-delay-of-first-starliner-crew-capsule-test-flight-to-august/

>> No.10518565

>>10518561
Related to
>>10518005

Hahahaha fuck Boeing

>> No.10518572

>>10518561
I have faith in Boeing they have decades of experience in the field and are the american way to space.

>> No.10518575

>>10518572
>desperation: the post

>> No.10518580

>>10518575
A-at least American Women will set foot on the Moon for the first time using a Boeing rocket.

>> No.10518581

>>10518572
>Crew Dragon will never launch, Boeing is our only way to space.
>A-alright, Crew Dragon MAY launch, but only after a bunch of delays and long after Starliner too! H-ha I bet it'll blow up too
>O-okay so Crew Dragon MAY beat Starliner to launch b-but I bet there'll be some big safety issue! O-old space for life!
>Please just let Starliner launch. It'll do a good job, I swear.

>> No.10518588
File: 140 KB, 1850x684, 1551837307487.png [View same] [iqdb] [saucenao] [google]
10518588

>>10518581
>P-pls sir, let us lunch it to space
>We won't shut in it, me promise

Give it to the poos, it would be hilarious

>> No.10518590

>>10518588
*Shit

>> No.10518604

>>10518590
haha dogs

>> No.10518623

Congress should have downselected to one provider only as was intended.

>> No.10518651

>>10518561
This and the reveal that the Ethiopian pilots did everything the instructions said incase of MCAS fucking up and still crashing paints a grim image over Boeing.

>> No.10518670
File: 840 KB, 842x595, D0K4eRuX4AA6v39.png [View same] [iqdb] [saucenao] [google]
10518670

>>10518089
Is there a reason why russians and europeans assembly Soyuz differently?
In Guiana they usually install payload after rocket already stand vertically on launchpad, while in Baikonur that install payload horizontally in assembly building.

>> No.10518681
File: 321 KB, 1309x1230, mars-travel-time.jpg [View same] [iqdb] [saucenao] [google]
10518681

>>10518364
It all depends on how much dV you add, and how much you trust your spacecraft. But mostly it depends on the relative positions of Earth and Mars orbits.

>> No.10518684

>>10518651
>everything the instructions said
All because the folks at Boiiiiing! had such a hard on for type certification that they wouldn't even mention MCAS in the official documentation. Western-world pilots apparently knew about it and how to bypass it anyhow.

>> No.10518696

>>10518364
6 months is actually the average reduced travel time trajectory, a Hohmann transfer takes more like 8 months on average and can take over 9 months.

>> No.10518697

>>10518561
If it's Boeing it ain't going

>> No.10518698

>>10518696
Nice lie bro

>> No.10518699
File: 905 KB, 220x220, Blank+_2f28248c7f6e31e1ed2b5e681742b533.gif [View same] [iqdb] [saucenao] [google]
10518699

>>10518698
I aint lyin bro

>> No.10518703

>>10518699
Want to provide a source then?

>> No.10518740

>>10518651
Boeing is a moribund company trying to relive it's golden age past. Now it mainly victimizes the US taxpayer by padding it's income with our money to build non-innovative boondoggles for the us government

>> No.10518901

>>10518740
Bunch of stick-pushers, that's what they are

>> No.10518922

get in here! NASA FY 2020 budget request review: https://www.youtube.com/watch?v=KhewOOUevDY
We might find out if SLS is really BTFO.

>> No.10518937

>>10518922
oh wait I fucked up, it's not live.

>> No.10518939

>>10518922
>mountain dew
that's from yesterday

>> No.10518987

>>10518696
Correct. Hohmann transfer to Mars (the lowest fuel consumption transfer) is 8-9 months.

However, if you optimize for least travel time as will be the case for manned missions, and have plenty of delta-v to spare (and fully refueled Starship will have around 9km/s), then the transfer takes 3-5 months.

6 months is what your usual probe sent to Mars takes, which is optimized for both aspects.

>>10518681

>> No.10519130

>>10518588
I think Boeing's space activities are one of the least poo-fied positions for obvious reasons

>> No.10519132

>>10518987
>>10518681
what the fuck did we need to go from chemical to nuclear rockets to get any faster travel times?

what do we need for a 1 month manned voyage to mars?

>> No.10519146

>>10517777
wasted

>> No.10519236
File: 231 KB, 2048x1365, 01-emdrive-update.jpg [View same] [iqdb] [saucenao] [google]
10519236

>>10519132
>what do we need for a 1 month manned voyage to mars?

>> No.10519269

>>10519236
Nice memedrive

>> No.10519385

>>10518670
westerners have a hardon for vertical assembly
the Soviets never gave a shit about that, which continues to Roscosmos

>> No.10519413

>>10519269
can't spell emdrive without memedrive

>> No.10519464

>>10519132
You'd need some kind of supper efficient scifi engine that doesn't exist, or an unrealistically massive transfer vehicle with a fuck ton of delta v.

>> No.10519500

>>10519413
Its name speaks for itself.

>> No.10519502

>>10519464
>>10519132
All you need is a big fucking laser and the ability to make lightweight mirrors. If you want your passengers to survive the journey, you need two big fucking lasers.

>> No.10519673

Arabsat 6A weighs 6,000kg. Falcon 9 is cabable if throwing 8,300kg to geostationary transfer orbit in expendable mode. So why is Falcon Heavy being used for this launch?

>> No.10519676

>>10519673
contract was signed for Falcon Heavy many years ago, and Falcon Heavy and Falcon 9 have both gotten much stronger over that time period

>> No.10519692

>>10519236
any updates on Cannae/EM drive

>> No.10519709

>>10519692
fake news, apparently

>> No.10519712

>>10519692
it's a meme

>> No.10519716

>>10519709
>>10519712
say it ain't so

>> No.10519718

>>10519716
unfortunately, reactionless drives aren't real yet

>> No.10519722

>>10519718
Such a shame, the very existence of some engine that would close the distance from Earth to Mars at 30 days or so would be world changing

Hell on such a drive the Moon could be reached in a day or less, imagine traveling to the Moon like we travel to other countries now, no more than 24 hours

fuck

>> No.10519829

>>10519673
Expendable mode.

>> No.10519887

>no mercury fueled MPDs
>no nuclear pulse propulsion
>not even NTRs
we're never gonna make it bros, we lost the edge

>> No.10519931

>>10519722
Dude even if it worked it's power requirements for even millinewtons of thrust were so ridiculous that it would be substantially slower than even chemical rockets.

>> No.10519961
File: 97 KB, 789x823, 1521770775307.jpg [View same] [iqdb] [saucenao] [google]
10519961

>>10519931
lets just build a nerva already and get some fast spaceships going

6 months to a planet is unacceptable

>> No.10519983

why the hell is SLS such a shitshow anyway?
do we really just have to accept that NASA built a heavy-lift rocket 50 years ago but they can't do it today?

>> No.10519986
File: 13 KB, 220x279, Richard_Shelby,_official_portrait,_112th_Congress.jpg [View same] [iqdb] [saucenao] [google]
10519986

>>10519983
Because the primary purpose of SLS has always been the distribution of government pork.

>> No.10520005

>>10517150
looks like timber rafting

>> No.10520013

>>10519986
Fortunately they are pretty close to importing enough Mexicans to get this cunt out of office

>> No.10520029

>>10516266
question has this sort of top heavy configuration been tried before, (I know spacex lands rockets, and makes steel ships in the middle of fuck all texas lighting shit on fire)
But point still stands is there a technical precedent for this? I assume it works out on paper atleast?

>> No.10520038

>>10519722
yeah, it's a shame perpetual motion machines don't exist

>> No.10520056

>>10520029
we don't know

>> No.10520111

>>10519983
SLS is ultimately not about making an launching a rocket, but giving money to key contractors.

>> No.10520174

>>10517031
More like why not just fucking fly it across country

>> No.10520175 [DELETED] 
File: 494 KB, 760x749, 77vYy7JSf.png [View same] [iqdb] [saucenao] [google]
10520175

>>10516182

>> No.10520189

>>10516182
>Highwind.mp3 plays

>> No.10520199
File: 156 KB, 320x210, of happenings.gif [View same] [iqdb] [saucenao] [google]
10520199

https://twitter.com/nextspaceflight/status/1113606676274384903

>> No.10520220

>>10520199
Can't see shit son, looked successful though.

>> No.10520222

FUCK OH FUCK I'M MAKING A WEBM RIGHT NOW EVERYONE STAY CALM

>> No.10520224

>>10520199
Thought it would look more blue

>> No.10520226

>>10520199
IT BEGINS

>> No.10520227
File: 172 KB, 606x454, 7e60cccbe440cb652d5ef040bf81ef66.jpg [View same] [iqdb] [saucenao] [google]
10520227

>>10520224
the red color is from the burning concrete

>> No.10520232

>>10520224
The direct exhaust is very blue if you watch the test stand fire, this is the exhaust burning all the random shit on the ground

>> No.10520234
File: 2.15 MB, 1442x844, fire-2.webm [View same] [iqdb] [saucenao] [google]
10520234

>> No.10520236
File: 1.23 MB, 966x652, fire 2.webm [View same] [iqdb] [saucenao] [google]
10520236

>> No.10520240

>>10520234
>>10520236
WHAT IS THIS POTATO SHIT ITS FUCKING 2019 WHERE IS THE 4K FEED

REEEEEEEEEEEEEEEEEEEEEEEEEE

>> No.10520243

https://twitter.com/elonmusk/status/1113613409767964673
"Starhopper completed tethered hop. All systems green."

>> No.10520246
File: 198 KB, 1178x508, GREEN.png [View same] [iqdb] [saucenao] [google]
10520246

>GREEN

>> No.10520252

>>10520199
IT BEGINS
>>10520240
it's a webcam that's located far away from the site

>> No.10520255

>>10520220
>>10520234
>>10520236
>>10520240
For real, where is the dank SpaceX feed? Are they going to do them once it starts hopping properly.

>> No.10520260

>>10520255
Grasshopper didn't livestream. They only showed the highlight videos afterwards, and the hopper that exploded was barely acknowledged until the blooper video. Knowing them now, it'll be the same with this hopper except uploaded to Twitter/Instagram instead of Youtube.

>> No.10520261

>>10520240
a local by the name of BocaChicaGal has a really good remote video camera on the ground at the launch site, and we'll have really good video of that (better on NSF L2, but L2 anon will need to be around still for that) like tomorrow or something
so be patient
unless Elon blesses us with another tweet

>> No.10520267
File: 3.38 MB, 4774x3299, IMG_4481.jpg [View same] [iqdb] [saucenao] [google]
10520267

>>10520255
they have a shitton of cameras. Don't worry

>> No.10520277

>>10520267
Pretty sure those are spotlights anon

>> No.10520286

>>10520277
on either side are two spotlights but in the middle there's a webcam

>> No.10520297 [DELETED] 

>>10520240
>https://twitter.com/nextspaceflight/status/1113606676274384903
Go look at a map and see how far away South Padre Island is from the launch site. Spoiler: it's about 5 miles.
The webcam is using a telescope to see that far. And sometimes clouds love the earth so much they come down from the sky to hang out with it. It's called "fog".

>> No.10520300

>>10520240
Go look at a map and see how far away South Padre Island is from the launch site. Spoiler: it's about 5 miles.
The webcam is using a telescope to see that far. And sometimes clouds love the earth so much they come down from the sky to hang out with it. It's called "fog".

>> No.10520315

>>10517547
Because spacecraft are very complicated and have thousands of interdependent parts. It's not like putting Legos together.

>> No.10520326

>>10520300
>And sometimes clouds love the earth so much they come down from the sky to hang out with it. It's called "fog".
Why hasn't this bug been fixed yet

>> No.10520328

>>10520315
>t. Richard. 'SLS'. Shelby

>> No.10520342
File: 15 KB, 311x143, meme.png [View same] [iqdb] [saucenao] [google]
10520342

>>10520328

>> No.10520354

>>10520342
Smash that ok button folks

>> No.10520359
File: 57 KB, 1780x232, 0257.png [View same] [iqdb] [saucenao] [google]
10520359

heh

>> No.10520368
File: 69 KB, 2520x206, 796.png [View same] [iqdb] [saucenao] [google]
10520368

heheh

>> No.10520371

>>10520359
>>10520368
Based BFR collage poster, the day is getting closer and closer fren.

>> No.10520375

>>10520371
yee

>> No.10520382

>>10516266

>> No.10520387
File: 37 KB, 1280x720, im1.jpg [View same] [iqdb] [saucenao] [google]
10520387

>>10520199
They solved the icing problem!

>> No.10520398

should be getting official video in a few min

>> No.10520403

>>10520387
Practically overnight too, pretty amazing. Imagine how long oldspace would twiddle their thumbs over shit like this

>> No.10520412

https://www.youtube.com/watch?v=5vfiM10lc1M

Sounds a little bit flatulent, but it IS methane-fueled...

>> No.10520420
File: 1.45 MB, 2148x1172, noice.png [View same] [iqdb] [saucenao] [google]
10520420

https://www.youtube.com/watch?v=5vfiM10lc1M
https://www.youtube.com/watch?v=5vfiM10lc1M
https://www.youtube.com/watch?v=5vfiM10lc1M
https://www.youtube.com/watch?v=5vfiM10lc1M
https://www.youtube.com/watch?v=5vfiM10lc1M

>> No.10520423

>>10520412
now that's some good video

>> No.10520429
File: 1.22 MB, 1822x1368, speedy spool up.png [View same] [iqdb] [saucenao] [google]
10520429

h...he's fast!

>> No.10520450
File: 633 KB, 1434x666, NSF-2019-04-04-03-02-40-144.jpg [View same] [iqdb] [saucenao] [google]
10520450

#3 apparently

>> No.10520451
File: 1.86 MB, 1280x628, first hopper fire.webm [View same] [iqdb] [saucenao] [google]
10520451

here's a YT-DL -> webm of the fire from the good video

>>10520450
did they even ever test SN 2 before today?

>> No.10520454

>>10520451
I don't know, and anybody who does know isn't telling
I think they probably did but I'm guessing

>> No.10520459
File: 415 KB, 284x350, ice.webm [View same] [iqdb] [saucenao] [google]
10520459

icey

>> No.10520489

>>10520451
Hot damn

>> No.10520492

>>10520451
K I N O

I

N

O

>> No.10520495

>>10520451
three of those is going to be monstrous

>> No.10520516

>>10520495
Monstrously kino you mean

Fuck I am so hype

THREE ENGINE HOP WHEN

>> No.10520518

How are we supposed to deal with the excess radiation in space?

>> No.10520526

>>10520518
don't send people.

>> No.10520527

>>10520518
The most consistent fuck you up radiation comes from the sun, in the example of a BFR flight, there will be the mass of the engine bells, engine blocks, fuel tanks and cargo between the sun and crew which should be substantial enough to cancel out most of it except for flares in which case everyone piles into a storm shelter which will be a tiny box surrounded by shielding such as the water supply for the crew as well as heavy metals. As far as GCRs, nothing to be done about it, just a risk you have to take but all evidence points to it not being a huge risk over 6 months or so. There is no real way to stop GCRs short of metres of water/lead so it's just something people are going to have to suck up and deal with until we have sci fi fusion torch ships or whatever.

>> No.10520536

Absolute fucking awful week for SLS
>Boeing is full of fuck, schedule looks like it’s gonna slip again
>NASA growing impatient, EM-1 may fly on FH
>oh wait, we can add ICPS to FH, making SLS completely redundant
>starship prototype advances into flight testing

>> No.10520540

>>10520536
also
>europa clipper is a FH candidate
>LUVOIR has a new design config for starship

>> No.10520548
File: 82 KB, 800x600, 1553415660931.jpg [View same] [iqdb] [saucenao] [google]
10520548

>>10519961
something something nooclear bad because glowing green death goo that lasts forever or whatever the fuck
Were Nixon not an unbelievably colossal faggot that cancelled the program, we would have had boots on mars in fucking 1981
and were normies not gullible unthinking cattle, we would be considerably better off across the board in other aspects of life as well

>> No.10520550

>>10520326
we're still reverse engineering the program
we still haven't figured out how to open the command window to fix shit

>> No.10520551

>>10520375
I see a fourth fucking digit slot there
how goddamn many do you have

>> No.10520552

>>10520495
ASS BLAST
S
S

B
L
A
S
T

>> No.10520558

>>10520451
damn son

>> No.10520561

>>10520495
Imagine 32

>> No.10520579

>>10520561
>"future spacecraft will make this look like a rowboat"

>> No.10520588

>>10520550
This is what you get with fucking closed-sourced, undocumented software...

>> No.10520630

>>10520527
>just suck up and deal with it
it saddens me to think of all the cancer we'll be subjecting people to until we figure out something to combat this.

>> No.10520642

>>10520588
you are closed source, undocumented software.

>> No.10520655

>>10520642
>undocumented
not with a face book account

>> No.10520667

>>10520451
this is 1 engine. Wtf is the full configuration going to look like as it flies through the air. That thing fired for like 2 seconds.

>> No.10520687

>>10520199
dawn of a new space age

>> No.10520688

>>10520667
also I really doubt that was anywhere near full throttle

>> No.10520691

>>10520688
Could you even see it, as it launches? The sheer volume of bs it would kick up would be incredibly immense. Chad BFR, you'll see this shit for miles. A giant plume into the sky. What a dab

>> No.10520697

50/50 that either something broke or that tomorrow we'll have a long test

>> No.10520699

>>10520697
I agree, either shit's broke and going nowhere or brownsville is going to regret letting SpaceX set up shop where they did

>> No.10520702
File: 437 KB, 1663x1245, 5c72013807265.image.jpg [View same] [iqdb] [saucenao] [google]
10520702

>>10520699
people will complain about the noise 100%. Expect to see SpaceX-funded playground 2: electric boogaloo
https://www.wacotrib.com/news/business/spacex-nighttime-test-fees-pay-for-park-upgrades-in-mcgregor/article_7678f8b9-d3ae-5b56-b80f-4fdeed5a14a4.html

>> No.10520710

>>10520630
Most estimates put radiation doso of a Mars mission somewhere around 1 Sv, which means lifetime cancer risk increase of 5% or so (from 30% to 35%). It is not as big of a deal as people think.

Now if you want to have a colony with children on Mars, you better have underground habitats.

>> No.10520716

>>10520710
_____ ______

>> No.10520720

>>10520716
wat

>> No.10520730

>>10520403
>Inb4 boring flamethrower

>> No.10520733

>>10517101
It's not quite unrelated. The limit was set so existing missiles would fit on the Interstate Highway system, iirc.

>> No.10520741
File: 25 KB, 670x346, .jpg [View same] [iqdb] [saucenao] [google]
10520741

>>10520720

>> No.10520784

>>10520702
>it's SpaceX themed.
That' s very cute

>> No.10520839

Jesus the amount of hellfire from that tiny engine is fucking incredible

>The little brap when they cut off the engine

Hnnnnnng

FULL HOP WHEN

>> No.10520840

>>10520710
>1 Sv
Not an expert here, but isn't exposure to 1Sv lethal?
If taken during a lifetime, it might just mean higher cancer risk, but 1Sv during a few months, that sounds like too much.

>> No.10520842

>>10520840
>>10520710
Some context:
ICRP recommendations from 1991: 0,05 Sv per year, 0,1 Sv per 5 years, 0,4 Sv per lifetime

>> No.10520848

>>10520840
it’s not a linear correlation

>> No.10520850

Anyone have a sound clip from 6-8 miles out? Lots of people on FB said they could hear it

>> No.10520854

it’s the world’s simplest thrust plate. If the hopper lifts off, then the raptor generated enough thrust to overcome the weight of the hopper itself

>> No.10520855

say what you are gonna say but mars will create a new wave of a-rad drugs. Or some new sick suits, or rad absorbant materials. Who really knows. Necessity is the mother of inventions.

Besides anyone born on mars will already be a lanklet, extra cancer is a fine trade off.

>> No.10520863

>>10520855
Cancer won’t be an issue in 20 years.
medical science is advancing still

>> No.10520867
File: 111 KB, 780x585, Stalker_ddbb1f_4322579.jpg [View same] [iqdb] [saucenao] [google]
10520867

>>10520855

>> No.10520868

>>10520839
see
>>10520450
Once that is lodged in the ass, then it will blast

>> No.10520875

>>10520868
SN 4 is needed. Can’t have uneven thrust, there are only three slots in a line for raptors on the hopper

>> No.10520878

>>10520875
What happened to SN2? Or is that the one in the hopper and they fucked the first one?

>> No.10520894

>>10520878
SN 1 was damaged https://twitter.com/elonmusk/status/1098653939141009408?lang=en
SN 2 has changes and is in the hopper right now https://twitter.com/elonmusk/status/1104945142065070081?lang=en https://twitter.com/elonmusk/status/1098656849740451840?lang=en

SN 3 will likely be the next one in, but SN 4 is needed for the full three in a row config to fully populate hopper with engines

>> No.10520908

how quickly can they assemble raptors? 32 is a fuck ton. If they lose a starship, it seems that things get sketchy. How much money can they have if they ever lose a starship. So much complicated, and difficult plumbing and high end engines.

>> No.10520924

>>10520908
not very fast, but they'll improve it once they figure out all the steps and can streamline the assembly line
the first few after the prototyping stage always take a long ass time

>> No.10520928

>>10520894
Cool, I figured that was the case, thanks anon.

>>10520908
At the moment seems a little slow but still pretty fucking fast compared to oldspace. This will get much, much faster as the design is standardised and they can crank them out assembly line fashion. Look at how fast they produce Merlin's and expect the same timeframe or quicker for raptors as the demand grows.

>> No.10520935

>>10520908
These machines are simpler than a modern turbofan.There was no reason why production took months and years other than idiotic oldspace practices.Spacex was/is building merlins in just a few days

>> No.10520969
File: 10 KB, 319x316, 1326659766401.jpg [View same] [iqdb] [saucenao] [google]
10520969

>>10520536
>oh wait, we can add ICPS to FH, making SLS completely redundant
Why stop at ICPS? EUS on Falcon Heavy soon, brothers!

>> No.10520974
File: 103 KB, 600x315, a.png [View same] [iqdb] [saucenao] [google]
10520974

>>10520702
>reusing so much that you reuse your playground design for your interplanetary rocket ship

>> No.10520983

>>10520908
They're literally just coming out of RnD and they have no real use for them yet outside of more RnD on Starhoppers. So obviously they won't get started on the full assembly line process cranking out dozens of engines quite yet. They'd just clutter up the place.

>> No.10521003

>>10520983
>>10520935
thanks boys, that gives me hope

>> No.10521097

>>10520029
Top heavy is better for rocket stability. The worst thing for stability is a very large mostly empty fairing, as it has a large surface area but low density, which means in flight dynamic forces are fighting to flip the rocket end over end.

>> No.10521111

>>10520688
If it was it'd lift the Hopper off the ground pretty fast, they probably started it up at minimum throttle and started throttling up for a couple seconds, and as soon as the feet left the ground they cut the engine.

>> No.10521112

>>10520691
The point of a launch pad is to limit all the debris of a launch to just water vapor from the sound suppression system and exhaust gasses from the rocket.

>> No.10521117

>>10520842
Correct, and they obviously aren't going to recommend a radiation dose that will knowingly result in an increased cancer risk. Basically what those numbers are are targets for background radiation levels for any manned outposts on the Moon/ Mars/Callisto/Asteroids, since you're going to be spending a long time there and you have the bulk material resources needed to provide shielding.

>> No.10521122

>>10520855
Rad drugs only work if there's radioactive elements in the environment (iodine pills blast your ass with non-radioactive iodine and thus prevents your body from absorbing the radioactive iodine that comes out of nuclear reactions, for example).

You can't take any drugs to save you from cosmic rays, all you can do is treat the damage they cause. If we ever cure cancer then cosmic rays become literally not a problem anymore, for any total dose, but until then the risk is there.

>> No.10521157

Progress 72 launch in Baikonur live stream
https://www.youtube.com/watch?v=21X5lGlDOfg

>> No.10521170
File: 952 KB, 2136x3216, Soyuz_TMA-9_launch_big.jpg [View same] [iqdb] [saucenao] [google]
10521170

>>10521157
4 minutes to launch

>> No.10521180
File: 1021 KB, 1920x1080, progress_2.png [View same] [iqdb] [saucenao] [google]
10521180

Looking good so far, if anyone interested.

>> No.10521199

>>10520699
I thought the original agreement was for 12 launchers per year from Boca Chica. I didn't think McGregor-tier testing was part of it. Anyhow, South Padre better get their ass in gear and build those viewing bleachers at the camper park already.

>> No.10521298
File: 665 KB, 2048x1755, FH,BLOCK5.jpg_large.jpg [View same] [iqdb] [saucenao] [google]
10521298

ITS UP

>> No.10521301

>>10521298
With no payload, so it's coming back down again

>> No.10521334

>>10520710
except all our studies on radiation dosage are pretty much useless for GCR exposure. GCR are quite different in the damage they cause.
>>10520855
Making antirad drugs and thin materials capable of absorbing radiation might turn out to be impossible.

>> No.10521346

>FH2 vertical
>Hopper fired
Today is looking good lads

>> No.10521361

>>10521346
https://twitter.com/SpaceflightNow/status/1113693180476710912

>> No.10521367

>>/wsg/2777286
I slept for a bit and Hopper test happened. What a time we live in.

>> No.10521372

>>10521367
Three arrows for cross board links

>> No.10521374

>>10521367
>>>/wsg/2777286

>>10521372
Yep, missed one

>> No.10521393

>>10521298
>2019
>taking a picture of a picture
Also why doesn't it have the black interstage like Falcon 9 has?

>> No.10521413
File: 117 KB, 1299x546, Nixon nixes the space program.png [View same] [iqdb] [saucenao] [google]
10521413

>>10520548
fuck nixon

FUCK NIXON

>> No.10521426

>>10520420
BRAP

>> No.10521432

Elon’s at the pad

>> No.10521440

>>10521432
Is that good or bad, I wonder.

>> No.10521445

>>10521432
How do you know this

>> No.10521457

>>10521445
>inb4 selfie of Elon at the pad

>> No.10521468

Progress successful docked few minutes ago.

>> No.10521485

>>10521468
nice nice

>> No.10521512

https://www.geekwire.com/2019/amazon-project-kuiper-broadband-satellite/amp/

amazon throws their hat in the ring

>>10521445
a tallish man without his reflective vest was just being shown around the hopper

>> No.10521541
File: 201 KB, 1080x1576, 1553595767986.jpg [View same] [iqdb] [saucenao] [google]
10521541

Elon is in a SEC trial from 2 pm on. Far from a rocket launch pad.

>> No.10521549

>>10521541
Why the fuck would he need to show up at his own trial? He has lawyers for that

>> No.10521600

>>10521512
Great, another constellation is exactly what we needed...Bezos is really behind the curve on this front, by the time these start launching hundreds of Starlink, Telesat and OneWeb satellites will be in orbit which means the market will already be massively over saturated. Furthermore, we have yet to be provided with a reasonable revenue case for these constellations, so I'm thinking we're going to experience a repeat of the 1990s satellite bubble explosion. Also, this ignores Kessler syndrome and the fact that the FCC may not be too happy with another multi-thousand satellite constellation, stopping Bezos in his tracks.

>> No.10521637

https://www.nytimes.com/2019/04/03/science/israel-beresheet-moon.html
the israeli lunar mission completed entered lunar orbit today & is scheduled to land on the surface April 11th.

>> No.10521639

>>10521637
>the israeli lunar mission completed entered lunar orbit
*entered lunar orbit. i need to go to bed.

>> No.10521644

>>10521199
they're limited to 12 launch campaigns a year and each launch campaign is limited to a few hundred hours of closures

>> No.10521648

>>10521600
do you know how many people live in the country and aren't served by the big landline companies? it'll basically destroy Hughesnet's market share and expand beyond that because current satellite SUCKS

>> No.10521650

>>10521600
There can be millions of satellites and it wont cause issues if there's proper burnout phase. FCC satellites requirement includes burnout phase, so any possible amount of satellites is fine.

>> No.10521723

>>10521334
>except all our studies on radiation dosage are pretty much useless for GCR exposure. GCR are quite different in the damage they cause.

Nope, GCR exposure is well studied in such populations as frequent flyers, people living in high altitudes, or astronauts. Radiation is a concern but we know radiation will not stop a Mars mission, period.

>> No.10521766

Guys, I was trolling at first, but what if BFR flies before SLS?

>> No.10521769

>>10521766
no shit it'll fly first

>> No.10521787

>>10521769
I mean the full stack, and with actual payload.
Before they started building the hopper, I was confident it was not happening anytime soon, but seeing this can test fire last night really made me think.
Will NASA commit seppuku then?
They'd be in a world of shit, that much's for sure.

>> No.10521793

>>10521787
I think it might be orbital pretty soon, they're going to want to do a lot of testing of the heat shield

>> No.10521797

ArianeSpace Soyuz launch right now!

https://www.youtube.com/watch?v=9uTxZbbRsgY

>> No.10521801

>>10521766
It does not even matter. SLS may fly once before BFR. Then it will take another two fucking years to fly a second time..

SLS is simply not relevant.

>> No.10521802

>>10521766
I doubt BFR will fly before SLS. However, if it did, then I expect much stronger encouragement from non-pro-SLS parts of the government to get SLS rushed out. Also pro-SLS factions will most likely double down on advertising the benefits of SLS over BFR. Mainly how the SLS uses proven and safe hardware while BFR is new and somehow inherently unsafe.

>> No.10521809

>>10521802
I still doubt it too, but I'd say we're about 1 more delay from it being plausible.

>> No.10521814

>>10521802
I fully expect BFR to Shuttle comparisons

>> No.10521816

>>10521650
>one sat gets niggled by something we can't/aren't tracking
>it cascades with other sats
>oh god oh fuck
just because we can have millions does not mean we should, for the simple fact that the chance of kessler syndrome increases exponentially for every new sat
then you got shitters like the poos, who just blew up one of their own sats for dick waving, and have now put the goddamn ISS in danger, let alone the fucktons of other satellites on the debris path

>> No.10521818

>>10521809
You mean like the 2020 launch? If that gets delayed then it'll most likely just get pushed back to early 2021 and by then BFR would not have progressed as much. Considering how many political pot shots are beening taken at SLS nowadays, theres a sudden pressure to actually get a rocket done "on time" rather than line the pockets of Boeing.

>> No.10521819

>>10521802
>proven and safe hardware
SLS is literally all new hardware at this point.
Different boosters. Different assembly of core stage. Modified engines, granted they've been tested to death.

>> No.10521829

https://www.cnbc.com/2019/04/04/mackenzie-bezos-to-keep-25-percent-of-couples-amazon-stock-after-finalizing-divorce.html
yow

>> No.10521831

>>10521816
We have the capability to field billion satellites without issues if satellites have proper procedure to destroy their satellites properly.
Kessler syndrome is only an issue if rogue states/companies insert objects into orbit without alerting a space agency that properly documents/tracks trajectory. Once in orbit, if there's no erratic propulsion, the orbit is fairly deterministic thus predictive.

>> No.10521839

>>10521831
>orbits of a proper satellite are predictable
no fucking shit you colossal retard
the issue is those fleks of paint and lost bolts that can blow fat chunks off of the things they hit, which hit others and create more shrapnel, which makes more and more in a cascade
that's what kessler syndrome is

when shit breaks off, it doesn't despawn like a video game, it stays up there to fuck yet more things in the ass

>> No.10521840

>>10521829
there goes 36 billion dollars of potential BO money

>> No.10521841
File: 75 KB, 963x539, fh_orion.jpg [View same] [iqdb] [saucenao] [google]
10521841

>>10516266
How would that work without extending the launch tower?

>> No.10521844

>>10521819
so it's even more fucking worthless?
the whole goddamn point of SLS was to reuse shuttle hardware
if they're making everything brand new, they could have just fucking made a new rocket that was actually fucking useful

>> No.10521856

FH launch now likely Monday

>> No.10521858

>>10521839
If it becomes an issue, we can always zap it with lasers. Both are an equal prospect for coming to reality.

>> No.10521860

>>10521841
Are you suggesting that extending the tower is more expensive than SLS?

>> No.10521861

>>10521797
Goddammit stick to Frogspeak.
You're shaming all of us.

>> No.10521862
File: 90 KB, 500x303, merely pretending.png [View same] [iqdb] [saucenao] [google]
10521862

>>10521858

>> No.10521864

>>10521860
Well, seems like a lot of work for a single launch.

>> No.10521872

>>10521841
>ULA seething in the background
I have to say, that black cladding was a good idea.

>> No.10521880

>>10521864
something something billion dollar single use SLS mobile structure something something

>> No.10521886

>>10521844
While the major parts are "new", they're evolutions from parts that have assembly lines and expertise behind them. So, in theory, SLS would still develop faster than an entirely new rocket.

Emphasis on "in theory". In actuality, SLS isn't a rocket program. It's a jobs program, so it's developing slower than expected, because most of those jobs and money will be at risk once (or if) SLS flies.

>> No.10521894

>>10521886
They literally used a new process to just force tanks parts together instead of simply soldering them.
That thing is new as fuck.
Not sure how it's named.

>> No.10521901

>>10521880
Reusable launch pads are a meme. The amount of performance you lose from making ot reusable can compromise a mission (ex. Tyranny of the Launch Pad Equation). Plus SpaceX hasn't even proven yet that reusable launch pads are economically viable. The amount of money spent on refurbishing a launch pad is so great that you might as well buy a cheaper expendable launch pad. Supporters of reusable launch pads are leading spaceflight into a dead end and end up forcing other responsible launch providers (ex. ULPA United Launch Pad Alliance) to waste money.

>> No.10521912

>>10521894
Do you mean friction stir welding?

>> No.10521915

>>10521797
Why isn't SpaceX launching these satellites? Surely they are much cheaper than Soyuz.

>> No.10521916

>>10521894
I mean it's a cool technique and it has applications.
But in this case, it was not required at all.
Can the SLS project get any more sad?
>>10521912
Not sure. I saw it a million years ago, and from what I understood, they just used sheer force to get plates to stick together.
Now this was made a whole lot more complicated by the fact they were dealing with cylinders.

>> No.10521923

>>10521912
But yeah, I've seen a video of this technique, and I don't think that's what they were describing at all.

>> No.10521924

https://twitter.com/CNBC/status/11138610412161966

Elon is at the court

>> No.10521925

>>10521916
It's friction stir welding. Mishoud completely refit their plant to support this new way of welding.

I don't know if it's required. I do know that tanks welded via friction stirring tend to be much stronger than tanks welded by conventional means. But even if it were somehow necessary, it shouldn't have taken over 10 years to figure out.

>> No.10521932

>>10521925
Well, then, they just described it badly.
Think I saw it on NASA's website, though.
I guess it involves some force too.

>> No.10521938

>>10521925
>I don't know if it's required
Elon's team are just yielding the weld torch like there's no tomorrow, though.

>> No.10521939

>>10521924
that's not a tweet that exists

>> No.10521963

>>10521939
quiet goy, can't you see he's trying to FUD here
he needs those nickels and dimes from his days of shilling

>> No.10521981

>>10521963
Honestly, at this point, I don't know that any shilling will work.
What happened yesterday means Hopper is actually serious shit.
It fired for 3 seconds. It's important, because it higher than 1 second.
Also, it didn't just blow up.
SpaceX is showing us simple wielding techniques are all you need to go to Space.
Now everyone in old space is counting down to how fast they can do it again.
They'd be in a hurry to shut the fuck up.

>> No.10521993

>>10521963
>>10521939
https://twitter.com/CNBC/status/1113861041216196616

Link got messed up sorry

>> No.10522003

>>10521993
Most likely Tesla shit.
I don't really care until I see them on the used market, though.
But I've been noticing them, here in France, recently.

>> No.10522006

>>10522003
They're everywhere in California when I visited
don't go, by the way, shit state
I see them around my home state from time to time

>> No.10522034

>>10521981
Let me add, when this shit goes airbone, and gets back down, there will be a serious increase in anti-depressant medicine for some reason.
I mean, they had the technology, but they never used it to its potential.

>> No.10522043
File: 970 KB, 924x874, 1.png [View same] [iqdb] [saucenao] [google]
10522043

this is the "I'm going to win" look

>> No.10522051

>>10522043
Why is he going, though?

>> No.10522055

>>10522051
he's being respectful of the court system

>> No.10522058

>>10522051
he has no respect for the SEC

>> No.10522076

>>10522058
So it's about his stunt with buying back Telsa share thing?
I can understand where it was coming from, and it was ill advised sharing it through nigger twitter.
Now, a year or so later, we can judge it was not impactful at all, so I guess that's what he'll plead.

>> No.10522084

>>10522076
oh no, he's being charged with contempt of court for supposedly disrespecting that buying back Tesla shares thing

>> No.10522088
File: 81 KB, 1208x466, lol.png [View same] [iqdb] [saucenao] [google]
10522088

>>10522084
>>10522076
not exactly, this all stems from the SEC settlement to get approval for material Tesla tweets, which they say he violated

of course the SEC is being fucktards about it

>> No.10522090

>>10522084
Well, he's in deep then.
Not that it impacts SpaceX as this will never be on the market.

>> No.10522093

>>10522090
we'll find out and I don't think it'll affect SpaceX at all

>> No.10522094

>>10522090
He's said that SpaceX could go public once they have a large Mars base. That was a few years ago though

>> No.10522096

>>10522094
Yeah, but that's by 2050, even in Elon time.

>> No.10522101

RS-25 test soon
https://www.youtube.com/watch?v=21X5lGlDOfg

>> No.10522103

>>10522094
Also, we're faced with new problems.
What if Elon flees to Mars and don't want to pay his fee to SEC anymore?

>> No.10522107

>>10522101
Why, they literally have hours of tests so far.

>> No.10522117

>>10522103
what if he holds the world hostage via threat of interplanetary bombardment?
what if he overthrows the world order?

>> No.10522132

>>10522117
Nah, he'd need nukes. Not something your just come over.

>> No.10522135

>>10521413
remember anon, we would have been on mars in '81 if it weren't for nixon. thank god he axed the budget, that'd be such an awful future.

>> No.10522138

"SpaceX may pause testing at the site for up to 60 days after the current round is complete. The company did not confirm a specific timeline once current testing objectives are complete"

booooo
https://www.brownsvilleherald.com/news/local/testing-closures-within-the-law/article_0b67ba8a-56e8-11e9-a008-c70420d80cb5.html?fbclid=IwAR3Lx5ZuoEh2CZI1wxzKo8jDuYnRK1ZEBx034P0rgtr3R39BOrgXMLYVH6o

>> No.10522141

>>10522132
orbital/interplanetary bombardment is a sufficient WMD desu

>> No.10522151

>>10522141
Nah, terminal velocity is a thing, even for sharp objects. Unless you launch them from the moon, but then you get a half week delay.

>> No.10522153

>>10522138
Oh noes, we agreed to a launch site, but we didn't expect loundness!

>> No.10522154

>>10522151
dumbass, launch them from Mars

>> No.10522157

>>10522154
>9 month delay.

>> No.10522161

>>10522157
>implying Earth would piss off Mars at the best part of the transfer window

>> No.10522162

>>10522157
three month, less if you really get it moving
and limited return strike capability
send it down around venus and you can approach from the sun so they'll never see it coming

>> No.10522168

>>10522161
Yeah, that was a best case figure.
And anyways, damage from a kinetic bolt wouldn't be that much.
With month warning, you can just fucking evacuate.

>> No.10522180

>>10520412
>>10520451
hopefully someone can do a webm with synced audio, the cameras are very far away so audio lags far behind

>> No.10522181

this SLS/RS-25 hype video fucking sucks
>>10522168
you could still blow up DC or Huntsville
you don't target people with that stuff, you target infrastructure, this was a lesson known by the IRA during the troubles

>> No.10522184

>>10522162
That's so retarded.
Imagine a game where it takes weeks for your shot to hit the enemy.
What will they do?
Did you see the matrix?

>> No.10522187

>>10522181
>BIGGER THAN A COMPACT CAR
>73 TIMES FASTER THAN A RACE CAR
>WOW WE MADE SIXTEEN (16) OF THEM
>MARS
>JOBBBBS

>> No.10522188

>>10522181
Nah this would take significant mass throw.
It's actually not a real threat.

>> No.10522189

>>10522103
>What if Elon flees to Mars and don't want to pay his fee to SEC anymore?
It's hard to take fiat currency with you when fleeing the fucking planet. Precious metals woudn't be as valuable as basic terrestrial chemicals like oxygen, carbon, and nitrogen.

>>10522132
>Nah, he'd need nukes. Not something your just come over.
Rods from God, m8.

>>10522135
>remember anon, we would have been on mars in '81 if it weren't for nixon. thank god he axed the budget, that'd be such an awful future.
Maybe if LBJ hadn't gotten us in to 'nam, things would be different. Maybe if LHO wasn't such a faggot and Kennedy survived his term, the Russkies might have landed on the moon first. After all, they did just about everything else in space first.

>>10522162
>three month, less if you really get it moving
They don't need reverse thrust to slow down, so you can add as much dV as you want, it just makes the boom bigger. But don't miss!

>> No.10522190

>>10522189
>Rods from God
Aka, the most inefficient weapon in history.
Everyone will just see it coming weeks in advance and just move away.
But maybe you should read the thread.

>> No.10522193

>>10522189
if only Korolev hadn't kicked it

>> No.10522198

>>10522190
>everyone will see it coming and just move away
that's a fucking good thing you retard, it lets you commit infrastructure terrorism without killing anybody

>> No.10522200

>>10522193
Play Battlezone 98 for a sniff of it.
What a great game it was.

>> No.10522207

>>10522198
Wew, that would get us nowhere.
Imagine negotiations when the shot has already been fired.

>> No.10522208

>>10522207
well, there are five more currently on the production line

>> No.10522213

>>10522208
Nah, I don't think so.

>> No.10522260
File: 55 KB, 1600x900, wojak.jpg [View same] [iqdb] [saucenao] [google]
10522260

Anyone baking?

I was at /pol/, Assad heard some rumors about /sg/ on /sci/. You better bake fast, he hates bakeries.

>> No.10522291
File: 19 KB, 867x236, Capture.png [View same] [iqdb] [saucenao] [google]
10522291

>>10522138
lol

>> No.10522300

So two Soyuz successfully delivered payloads to orbit today. Maybe Russia got their game back after all.

>> No.10522325

Hey /sg/, do you think that NASA will get people on the moon bu 2024?

>> No.10522326

>>10522189
>It's hard to take fiat currency with you when fleeing the fucking planet
Musk could easily use his favorite cryptocurrency Dogecoin from Mars

>> No.10522361

>>10522326
How do you update a blockchain with a 25 minute comms lag? But more important, there's nothing up there to buy, and if he bought something from Earth, the shipping costs would be "astronomical". Anything he left behind could just be seized to pay debts.

>> No.10522395

>>10522361
>How do you update a blockchain with a 25 minute comms lag?
You can easily send and receive crypto from Mars. Transactions can be signed offline without an internet connection and broadcast at a later time. For real time use the Mars colony would need its own blockchain though.

>> No.10522408

>>10522325
How long do you think it will take to develop and test a lunar lander? NASA is a giant bureaucratic hellhole...

>> No.10522436

>>10522408
Could a trimmed down Falcon 9 first stage land on the moon?

>> No.10522439

>>10522395
>For real time use the Mars colony would need its own blockchain though.
Or their own set of lightning nodes.

>> No.10522484

With all these MEO and LEO satellite constellations being launched is there really any rationale for geosynchronous comsats anymore?

>> No.10522486

>>10522436
No, the engines are too strong
Also you'd need to invent orbital cryogenic refueling first
And mitigate boiloff on the week long trip to the moon
Also the engines are not optimal for vacuum operation

>> No.10522497
File: 252 KB, 642x1448, Screen Shot 2019-04-04 at 3.37.46 PM.png [View same] [iqdb] [saucenao] [google]
10522497

>>10522291
relevant parts

>> No.10522505

>>10522486
>No, the engines are too strong
Right, a single Merlin is barely weak enough for Earth landings.
>Also the engines are not optimal for vacuum operation
I think the idea was making a version specifically for lunar landings, not re-using the core that got shit off of the planet. The use case for lunar landings is completely different than for a first stage. First stage boosters are to get shit out of our gravity well.
SS (without Heavy) should work for Mars and Moon landings.

>> No.10522558

>>10522484
no

>> No.10522571

>>10522486
>>Also you'd need to invent orbital cryogenic refueling first
Is that why we don't have refueling depots in orbit yet

>> No.10522572

>>10522300
Soyuz could fail ten times in a row and still be the safest ride to orbit in history.

>> No.10522587

>>10522571
You wouldn't need "refueling" with transfer hoses and shit if you simply left an attachable tank in orbit. Just swap tanks and you're good to go.

>> No.10522660

>>10521512
I'm having a hard time keeping count of all these new satellite constellations:
SpaceX/Starlink
OneWeb
O3b
Telesat
LeoSat
Amazon
US, Europe, China and Russia will probably launch their own LEO/MEO constellations to support military communications
Space is getting crowded. It's hard to imagine these tens of thousands of satellites all orbiting the earth at once.

>> No.10522661

>>10522571
With a large enough station you could actively cool the cryogenic fuel. You'd just need a lot of electricity and some big honkin' radiators.

The other problem is getting the fuel to flow from one tank to another in zero G. Theres a few ways around it, but the most efficient solution would be to have a spinning station for artificial gravity.

>> No.10522666

>>10522571
yeah
also fuel doesn't sit around forever, it boils off, so you can't keep it, so it needs to go right before the payload it's launching out of the Earth Moon system
so you can't put it up there waiting to sell it to the government for their interplanetary probes, and basically nobody's going to do it until they can be sure they have customers
and no customers are going to bank on a system that doesn't exist

>> No.10522669

>>10522661
it wouldn't even need to spin very fast, you could use pumps for the transfer, the spingrav is to make sure that all the boil-off bubbles and air pockets form in a consistent place

>> No.10522747

>>10522497
SpaceX is probably bringing more tourism to that backwater swamp shithole than ever before.

>> No.10522752

Time for new thread

>> No.10522755

>>10521413
NIX'D

>> No.10522786

>>10522752
make sure the OP is an absolute shitpost

>> No.10522790

>>10521938
>>10521925
Falcon 9 is also friction stir welded, the fact that people point to SLS delays as being caused in part by using friction stir welding is laughable.

>> No.10522819

>>10522790
>Falcon 9 is also friction stir welded
Interesting! I didn't know that.

>the fact that people point to SLS delays as being caused in part by using friction stir welding is laughable
I forgot which /sg/ thread it was, but there was someone there who argued that the main reason why SLS is taking so long was because of the core tanks. Apparently making a tank that can handle the force of four RS-25s and 2 SRBs is such a herculean task that justifies the 10+ years and nearly $14B.

I know tanks for rockets aren't just a simple pressure vessel that holds fluids, but they are significantly simpler than liquid propellant engines and solid motor boosters. It shouldn't take that long to figure out how to make a reasonably lightweight tank that can handle the forces involved in SLS.

>> No.10522906

>>10522819
Designing a tank is actually very simple. You just compute how large it needs to be, how much it will weigh when full, what the maximum internal pressure will be, what is the maximum thrust it will be subjected to, and what the maximum expected bending loads will be, then build a cylinder with that volume and walls thick enough to take the compression loads, with some stringers to increase stiffness.

>> No.10522949

New thread

>>10522947
>>10522947
>>10522947