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/sci/ - Science & Math


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File: 392 KB, 2048x1536, IMG_3702.jpg [View same] [iqdb] [saucenao] [google]
16044380 No.16044380 [Reply] [Original]

Lunar (IM)age Edition

Previous - >>16041984

>> No.16044391

>>16044371
What did anon mean by this

>> No.16044404

>>16044380
Still no pictures??

>> No.16044407
File: 264 KB, 592x471, im-1.png [View same] [iqdb] [saucenao] [google]
16044407

https://twitter.com/coastal8049/status/1761861522676928661
>It means that most of the IM-1 antenna's signal is bouncing of the Moon's surface to get to us. IM-1 is natively RHCP and when that signal reflects off of something it becomes LHCP. Meaning the direct signals from IM-1 are largely blocked.
lmao

>> No.16044408

>>16044391
If you can see a daylight planet surface, your eyes will be day-adjusted and you won't see stars.
It's not completely true because your eyes have better range than a camera, but it's realistic for cameras

>> No.16044413

>>16044407
Thay fell inna fuckin hole m8

>> No.16044414

https://www.youtube.com/watch?v=UjPGONm5bNM
Starlink happening in T-19:00

>> No.16044415
File: 84 KB, 933x681, 1697562164011399.jpg [View same] [iqdb] [saucenao] [google]
16044415

>>16044404
no pictures = no stonks!

>> No.16044418
File: 89 KB, 1007x732, 1678471443621836.jpg [View same] [iqdb] [saucenao] [google]
16044418

>>16044415
updated

>> No.16044420

>>16044418
>>>/biz/

>> No.16044423
File: 128 KB, 2500x1667, 1683560917910213.jpg [View same] [iqdb] [saucenao] [google]
16044423

>>16044420
without /biz/ we'd be relying on starliner to get to orbit

>> No.16044425

House China committee demands Elon Musk open SpaceX Starshield internet to U.S. troops in Taiwan
>The House Select Committee on the Chinese Communist Party sent a letter on Saturday to Elon Musk demanding that U.S. troops stationed in Taiwan get access to SpaceX's Starshield, a satellite communication network designed specifically for the military.
>The letter, obtained by CNBC and first reported by Forbes, claimed that by not making Starshield available to U.S. military forces in Taiwan, SpaceX could violate its Pentagon contract, which requires "global access" to Starshield technology.
https://www.cnbc.com/2024/02/24/house-china-committee-elon-musk-spacex-starshield-taiwan.html

>> No.16044430

>>16044423
Ya now go talk about it there

>> No.16044443

>>16044423
Get the fuck out of here

>> No.16044450

>>16044425
SpaceX has never provided internet service to Taiwan because Taiwan does not allow them to.

>> No.16044451

>>16044425
>+11 I’ve been wondering if musk is compromised by China. This only supports that idea
https://www.reddit.com/r/technology/comments/1azxqzc/spacex_may_be_withholding_satellite_internet_in/

>+38 Surely, with all the money and resources available to them, the US military can create their own Starlink alternative and take that shitbag Musk out of the equation?
>+15 Just remember, Elon. They can take your shit if they want to because 'national security'.
https://www.reddit.com/r/technology/comments/1azuk7w/us_lawmakers_are_calling_on_elon_musk_to_make/

literal hitpiece designed to turn public opinion further against elon, spacex, and spaceflight. they want to keep us trapped on this prison world until we're all fried to death from global warming that they created.

>> No.16044452

>>16044450
US troops in Taiwan
not to taiwanese citizens....

>> No.16044457

>>16044451
https://www.reddit.com/r/EnoughMuskSpam/comments/1azc2kt/exclusive_lawmakers_demand_elon_musk_provide/

>> No.16044473

>>16044414
Falcon 9 does it again

>> No.16044474

>>16044451
Kys redditcel

>> No.16044476
File: 36 KB, 720x720, 1687428829369831.gif [View same] [iqdb] [saucenao] [google]
16044476

>>16044407
What's the point or retroreflectors if we can trasmit signals and read them by simply bouncing them off the Lunar surface?

>> No.16044481

The new holy grail of rocketry
https://youtu.be/KX-0Xw6kkrc

>> No.16044482

>>16044452
>US troops in Taiwan

Think about that for a second.

>> No.16044486

>>16044482
Okay, I did some thinking. What now?

>> No.16044487

>>16044482
think about what? we have troops in taiwan. we've had them there for years.

>> No.16044490

>24 starlinks
nice
improvements

>> No.16044492

>>16044487
Name the unit stationed in Taiwan.

>> No.16044493

>>16044492
Army Green Berets of the 1st Special Forces Group
https://www.newsweek.com/american-special-forces-train-taiwan-soldiers-penghu-kinmen-china-coast-1868009

>> No.16044497

>>16044493
I asked you which unit was stationed in Taiwan, not whether a handful of US personnel were acting as instructors for the Taiwanese army.

>> No.16044499

>>16044497
nobody said stationed, you just brought that up in order to move the goalpost

>> No.16044506
File: 174 KB, 1200x1111, sas-1.jpg [View same] [iqdb] [saucenao] [google]
16044506

Really im supposed to believe this shit can land on the moon after what we saw with nova C? This is extremely dangerous and useless. Even the minimun error could tip it over, Artemis IIIs astronaust are even in a worse situation than starliners

>> No.16044507

>>16044481
fucking love this guy, I found him after the algorithm recommend me his discussion of the F-14 Tomcat's microprocessors

>> No.16044509

>>16044506
skill issue

>> No.16044513

>>16044506
You can always just abort and fly back to orbit if you have too much translational velocity or closure rate or whatever. It's that easy in rocketry when you have return fuel with you.

>> No.16044515

>>16044506
This thing is going to strand the Artemis-III crew on the moon, they better send extra consumables.

>> No.16044522

>>16044476
lunar surface isnt a mirror, it would scatter the light

>> No.16044524

>>16044506
nova C forgot to turn their lidar on. using unfamiliar instruments as a back up is probably the source of the issue and not vertical landings themselves.

>> No.16044526

>>16044506
wtf does Nova C have to do with it?
You're comparing a little bundle of junk parts with a rocket that has engines and half-full tanks that give it a low CoW.
Have you ever wondered why F9 stages don't fall over on the barge? That's because it's a fucking empty soda can with rocks on the bottom.

>> No.16044532

>>16044522
Light is a wave, though

>> No.16044539
File: 15 KB, 1228x592, moon.png [View same] [iqdb] [saucenao] [google]
16044539

>>16044532
my understanding of how they work

>> No.16044540 [DELETED] 

>>16044526
Nova-C also has engines and half-full tanks...?

>> No.16044541
File: 662 KB, 330x246, Reflection-coin-cube-rot.gif [View same] [iqdb] [saucenao] [google]
16044541

>>16044476
https://en.wikipedia.org/wiki/Corner_reflector
because it's a corner reflector that always reflects back to the source

>> No.16044546 [DELETED] 
File: 159 KB, 2047x1152, 2023-08-16-image-3.jpg [View same] [iqdb] [saucenao] [google]
16044546

>>16044526
>that has engines and half-full tanks
Nova-C also has that though?

>> No.16044549
File: 459 KB, 1x1, 1678834123239472.pdf [View same] [iqdb] [saucenao] [google]
16044549

>>16044539
>>16044541

Consider the following

>> No.16044554
File: 159 KB, 2047x1152, 2023-08-16-image-3.jpg [View same] [iqdb] [saucenao] [google]
16044554

>>16044526
>that has engines and half-full tanks
Nova-C should be even better in that regard, in that it has the engine but the tanks above are almost completely empty

>> No.16044555

>>16044546
>>16044554
>no common bulkhead
Why?

>> No.16044558

>>16044555
$$$ I'd guess

>> No.16044568
File: 452 KB, 2896x4096, 1608125348287.jpg [View same] [iqdb] [saucenao] [google]
16044568

>>16044546
>>16044554
>npc can't imagine the apple in his head
>npc can't imagine the inside of a rocket and where the heavy parts are
>thinks the can walls and a few toys at the top are heavier than half a tank of LOX
>thinks he knows something that hundreds of SpaceX geniuses have overlooked
>many such cases
take a soda can, drink half the soda, then try to tip it over by poking at its top edge with your finger, bonus if you drop some marbles in there too to represent the engines

>> No.16044569

>>16044506
Easy
Just don't hit any roggs

>> No.16044583

>>16044568
It's more like two half-empty cans stacked on top of each other. But that is beside the point.

Imagine if the can was fully empty of liquid, and instead of the liquid you put more marbles of equivalent mass into it. That is Nova-C

>> No.16044584
File: 535 KB, 1108x1613, a IM-1-MOON-EAGLE-CAM-01 plan b.jpg [View same] [iqdb] [saucenao] [google]
16044584

In desperation to salvage something from the crashed IM-1 moon didn't lander, the mad lads at EagleCam are going to Super Mario Jump their mini probe off the bent bird:

> “We are currently running simulations which show that EagleCam should deploy a total distance of somewhere between 3 to 5 meters [10 to 16 feet], with a best guess at about 4.1 meters [roughly 13 feet],” said Troy Henderson, faculty lead of the EagleCam team.

Pic related.

>> No.16044587

>>16044584
How will they transmit the footage back to Earth?

>> No.16044594

>>16044584
Why didn't it deploy during landing when it was supposed to, wasn't that the whole point?

>> No.16044596

>>16044587
wifi

>> No.16044597

>>16044549
Final statement:
>According to the number of return photons I go even further and conclude that in all lunar laser ranging experiments the measurements were taken to the bare surface of the Moon.
the data does seem to fit that interpretation. interesting find

>> No.16044599

>>16044594
I believe they unscheduled the EagleCam deployment when they reprogrammed the lander to use the payload doppler lidar

>> No.16044600

>>16044415
>>16044418
its ogre...

how will spacex land if the adults in the room cant?

>> No.16044602

>>16044583
You still don't seem to comprehend just how much denser the LOX is. Look closely at the numbers on that pic. The LOX is only a little bigger, but weighs 3.5 times as much as the CH4.
Now imagine that the bottom half of that soda can is full of mercury.
And even half full, the total of fuel is still clearly all in the bottom half of the rocket.

Wise man once say:
Weebles wobble, but they don't fall down.

>> No.16044603

>>16044596
That just lets them transmit to the lander, which can't even send back to Earth footage the lander itself takes

>> No.16044604
File: 160 KB, 2000x2000, punching bag 71HS-l6Q28L.jpg [View same] [iqdb] [saucenao] [google]
16044604

>>16044583

>> No.16044616
File: 1019 KB, 2539x1263, eaglecam-moon.jpg [View same] [iqdb] [saucenao] [google]
16044616

>>16044587
> “We have built-in redundancies into this device, with Wi-Fi antenna diversity both in the payload and the lander, which increases our chances of mission success under these unexpected scenarios,” adds Eduardo Rojas, the Embry‑Riddle assistant professor of Electrical & Computer Engineering who designed EagleCam’s Wi-Fi antennas.

Not so much a problem of getting signal back to the crashed lander, but the lander with low power and bad antenna orientation relaying that signal to Earth. And a yatzee roll whether the bot lands with the camera pointing the right direction.

>> No.16044617

>>16044602
>lox is denser than ch4
So? Both are denser than helium pressurant, no?

I don't see how it matters how dense the propellants are. It's still better to have the mass be mostly concentrated in the engine at the bottom, than to have a larger fraction of the mass in the tanks above it

>> No.16044621
File: 137 KB, 666x788, EAGLECAM-01.jpg [View same] [iqdb] [saucenao] [google]
16044621

"Wheeeee!"

>> No.16044626
File: 108 KB, 889x697, CSM-LM rendezvous & docking MOON apollo.jpg [View same] [iqdb] [saucenao] [google]
16044626

>> No.16044627

>>16044621
its so over...

>> No.16044629

>>16044506
>It might tip over
Isn't that why they're so adamant about sending the diversity team first?

>> No.16044635
File: 151 KB, 2048x1366, GHNomoEXIAEB7dO.jpg [View same] [iqdb] [saucenao] [google]
16044635

>> No.16044641

>>16044568
The header LOX tank sure has a lot more mass than I thought it would

>> No.16044648

>>16044635
This is the last time anyone's ever going to be seeing this, unless Japan actually decides to build the H3 Heavy.

>> No.16044661

>>16044648
Good, using hydrolox for your first stage is retarded.

>> No.16044664

>>16044452
Taiwan is a sovereign nation with its own laws

>> No.16044668

>>16044583
>>16044617
Anon, you're just going to have to accept that your eyes are not a good judge of physics, and leave it to the experts who have actual data and simulators.

>> No.16044673 [DELETED] 
File: 2.87 MB, 1920x1080, 1561445743742.webm [View same] [iqdb] [saucenao] [google]
16044673

>>16044506
Yeah it's tall and narrow so it can never land.

>> No.16044675

>>16044391
>typical gay astronomer
not worth worrying about

>> No.16044677
File: 2.89 MB, 1280x720, 1665547026964772.webm [View same] [iqdb] [saucenao] [google]
16044677

>>16044506

>> No.16044680

>>16044677
Yooooooooooooo

>> No.16044681

>>16044677
crazy how it do dat

>> No.16044686
File: 62 KB, 500x800, sKT2lkFLCg5n.jpg [View same] [iqdb] [saucenao] [google]
16044686

>> No.16044694

reminder, the upcoming crew-8 has Jeanette Epps, another one of the Boeing slated astronauts that got reassigned

>> No.16044700 [DELETED] 

>it's a Lisa episode

>> No.16044719

>>16044681
really it should be more crazy that other rockets don't do that.

>> No.16044722

>>16044719
2025 looks like it's going to be the year that the rest of the industry finally starts catching up to 2015 SpaceX.

>> No.16044739
File: 179 KB, 1024x768, 1024px-Astronaut_class_group_20.jpg [View same] [iqdb] [saucenao] [google]
16044739

>>16044694
must be brutal knowing that you graduated training in 2011, everyone else on your 14 person group has flown by now but you've still never left earth. not only that but the group after you has also all flown. even most of the group after them has no flown.

imagine telling everyone you're an astronaut for the past decade and a half and just waiting around at home.

>> No.16044767

>>16044739
We've always trained an absurd number of astronauts compared to the actual number of crewed missions

>> No.16044770

anyone else thinking we could probably massively improve tps tile performance if we made them from actual high temperature ceramics rather than fuckin silica?

>> No.16044772

>>16044767
well they managed to get through the rest of her group and the one after. the crew dragon really helped with that

>> No.16044774

>>16044739
Astronaut recruitment must have suffered greatly after the shuttle was retired

>> No.16044776
File: 215 KB, 675x1200, GHFgULEXQAErAMF.jpg [View same] [iqdb] [saucenao] [google]
16044776

What would happen if China make it to the moon before Artemis III? I Think itd be a hard blow to NASA, because to the eyes of the public/normies China would be the new biggest superpower in space, and its going to happen the same thing after apollo 11, no one gonna give a fuck about artemis III because the chinese did it earlier

>> No.16044777

>>16044770
no, actually I mostly think about how we could brute force our way into using cheaper crappier materials for everything.

>> No.16044778

>>16044776
Nothing, but it would be a black eye for a space program that declared a stated interest in doing something and proceeded to fail at doing it for decades

>> No.16044780

>>16044777
that can still be accomplished while alongside going to an all-alumina tile, for example.
hafnium carbonitride has a melting point of over 4000 celsius

>> No.16044781

>still no pictures
holy shit what a disaster

>> No.16044784

>>16044781
The only signal theyre getting is reflecting off of the moon. Its actually ogre, I wonder if they get to keep all that money they got.

>> No.16044790

>>16044784
money was mostly for the cost of the lander/rocket. theres probably not much profit left after they pay their staff. but IM-2/3 give them a chance to redeem themselves in NASAs eyes for future missions

>> No.16044805

>>16044418
oof ow my funds

>> No.16044813
File: 181 KB, 1269x715, GHO47R2aAAAayZc.jpg [View same] [iqdb] [saucenao] [google]
16044813

https://twitter.com/wulei2020/status/1761955237320134786
>GalacticEnergy recently completed an experiment for liquid-propellant rocket Pallas-1, which aims to meet the demand for large-scale constellation networks.It features 7 “Welkin” 50ton reusable liquid oxygen/kerosene engines in its first stage & can deliver 8 tons into LEO.

Chinese Falcon 9 v1.0 seems like it's coming along nicely

>> No.16044816

>>16044568
That LOX header at the top is retarded.
It impedes normal fairings and separable loads.

>> No.16044819

>>16044813
good for them

>> No.16044820

>>16044816
it's necessary for CoM reasons during reentry, if you're not coming back down you don't need it

>> No.16044823

>>16044820
That little tank cannot possibly outweight the raptors. The thing will reenter bottom-first in any case.

>> No.16044824

>>16044813
the virgin american workhorse rocket vs. the chad chicom purpose-built shitcan #46456764

>> No.16044826

>>16044823
that little tank weighs 25 tons

>> No.16044839
File: 31 KB, 1180x899, idea.png [View same] [iqdb] [saucenao] [google]
16044839

Would an orbit transfer station like this be possible? If you need access to Mars or Ceres/Asteroid Belt you can ride this thing until it gets there if its a large enough station i.e. self-sufficient with plant farms & artificial gravity (not O'Neill cylinders). Maybe you swing by the asteroid belt on the ship to pick up a load of materials from a mine and drop it off at Mars, grab a food resupply while there and head back to Earth to sell goods? I would think of it as the first real space 'ship' like how was done in the colonial period. Not sure how the gravity would work, it would probably be a bunch of joined rotational space stations with boosters attached and separate gravities for Martians, Terrans, Lunarians, Belters, etc. to get acclimate to any locations they get dropped off at. The thing I'm not sure if Earth's, Mars' and Ceres' orbits would synchronize to establish a permanent stable connection for a space station that can consistently go around that fast or if maybe something else could be used.

>> No.16044840

Eagle Cam bros?

>> No.16044842

>>16044840
Buckbroken, by me.

>> No.16044872

>>16044770
How do you make them lighter than just silica?

>> No.16044878
File: 23 KB, 857x754, Aldrin_Cycler_2.gif [View same] [iqdb] [saucenao] [google]
16044878

>>16044839
behold the Aldrin cycler. two stations in heliocentric orbit. one has a fast trip Earth -> Mars and then a long way back (where it would be unmanned) and the other has a fast Mars -> Earth. The fast part of the orbit is the bit closest to the sun.

I don't think it would effect the delta-v to get to mars because any craft would still need to match orbits with the station before docking, but it would cut down on redundant mass for habitation etc.

>> No.16044884

>>16044878
Ingenius, but couldnt you have allot more stations along their own cycler paths to increase cargo back and forth? I would assume they never cross considering how big space is

>> No.16044901

>>16044549
GOOD POST

>> No.16044902

>>16044513
How can you abort when the rocket is already tipped over?

>> No.16044906

I need more /sfg/tards using MSPaint for the ideas you all have. I want to see what youve been thinking up come on then send some in.

>> No.16044913
File: 29 KB, 659x274, 009659.jpg [View same] [iqdb] [saucenao] [google]
16044913

https://twitter.com/elonmusk/status/1762002982684721190

>> No.16044917
File: 354 KB, 1800x621, Apollo-16-station-10.jpg [View same] [iqdb] [saucenao] [google]
16044917

this post was made with shitty overpriced Xfinity in Las Cruces

>> No.16044919
File: 237 KB, 651x979, 009660.jpg [View same] [iqdb] [saucenao] [google]
16044919

>>16044913
https://twitter.com/longmier/status/1761998954944921955

>> No.16044921
File: 1.49 MB, 1536x2048, GHPgtKwaoAAWoLf.jpg [View same] [iqdb] [saucenao] [google]
16044921

>>16044919

>> No.16044923

>>16044902
>How can you abort when the rocket is already tipped over?
the same way your mom attempted to abort you even though you were already in the 3rd trimester

>> No.16044924
File: 327 KB, 1452x2057, GEtJk0vbIAA0u0h.jpg [View same] [iqdb] [saucenao] [google]
16044924

https://twitter.com/SLIM_JAXA/status/1761981979237732355
>Last night, a command was sent to SLIM and a response received, confirming that the spacecraft has made it through the lunar night and maintained communication capabilities!
SLIM lives!

>> No.16044927

>>16044924
Kill it

>> No.16044928

>>16044924
best news all week

>> No.16044929

>>16044924
based. I didn't think it was even designed to survive the night, being a landing demonstration and everything. The japs are really good at salvaging missions

>> No.16044934
File: 150 KB, 1112x1008, 009661.jpg [View same] [iqdb] [saucenao] [google]
16044934

https://spacenews.com/faa-commercial-human-spaceflight-regulatory-learning-period-nears-expiration/
>The FAA has argued in the past that the learning period should be allowed to expire, arguing that doing so would give the agency the ability to start the process of developing safety regulations while noting that enacting new regulations would be a process lasting several years, rather than immediately after the learning period expires.

>> No.16044940

>>16044934
If anyone is gonna meet this its SpaceX and F9. I dont think there should be an issue with this for other companies as well other than VG. I say let it ride and get rid of some unsafe companies in the process.

>> No.16044943

I want starship hls interior photos

>> No.16044945

>>16044924
Told you, lunar night is the biggest nothingburger of all time, on par with muh perchlorates and muh radiation

>> No.16044949

>>16044945
how's muh starship HLS landing thrusters sending dangerous dust into lunar orbit doing anyways?

>> No.16044955
File: 53 KB, 658x537, 009662.jpg [View same] [iqdb] [saucenao] [google]
16044955

https://twitter.com/SpaceX/status/1762015710770016537

>> No.16044956
File: 257 KB, 3240x2160, GHPvudMa0AANRRl.jpg [View same] [iqdb] [saucenao] [google]
16044956

>>16044955

>> No.16044959
File: 609 KB, 3580x2160, GHPvvnYaEAAdfdn.jpg [View same] [iqdb] [saucenao] [google]
16044959

>>16044956

>> No.16044961
File: 847 KB, 3544x2160, GHPvw8kb0AA5UG2.jpg [View same] [iqdb] [saucenao] [google]
16044961

>>16044959

>> No.16044962

>new booster
scary ngl

>> No.16044976

>>16044945
if your lander's electronics and batteries are designed are designed to survive the extreme cold

>> No.16044980

>>16044976
RTGs need to be proliferated

>> No.16044984
File: 59 KB, 660x647, 009663.jpg [View same] [iqdb] [saucenao] [google]
16044984

https://twitter.com/elonmusk/status/1762019803630563800

>> No.16044986

>>16044984
SSTO 1st stage is possible now, you can't convince me otherwise .

>> No.16044992

>>16044506
I imagine they're remember to flip on the laser thingy that helps it land.

>> No.16044994

>>16044584
>distance of somewhere between 3 to 5 meters [10 to 16 feet]
The whole space industry treats everyone like retards. If someone can't convert meters to feet in their head, does anything that's happening on the Moon matter in the slightest?

>> No.16044995

>>16044976
They are designed áre designed for it ^_^

>> No.16044996
File: 69 KB, 816x1056, GHP409TbkAApPQq.jpg [View same] [iqdb] [saucenao] [google]
16044996

https://twitter.com/wintonARK/status/1762027012414431635
>what begins as novelty
>becomes a nice-to-have
>becomes an expectation
>becomes a requirement

>> No.16044997
File: 33 KB, 655x399, 009664.jpg [View same] [iqdb] [saucenao] [google]
16044997

>>16044996
https://twitter.com/elonmusk/status/1762029884048838721

>> No.16044998

>>16044997
this comes to mind as a recent example, hiker was just a couple miles from the trail but couldn't text anyone and died. https://www.theguardian.com/us-news/2016/may/26/hiker-who-went-missing-on-appalachian-trail-survived-26-days-before-dying

>> No.16045000

>>16044998
that is the exact example in the washington post article
went to take a leak and lost the trail, just got very unlucky I guess
or maybe she was retarded lol

>In a notebook entry dated 6 August 2013, two weeks after she lost her way, Largay made a desperate plea: “When you find my body, please call my husband George and my daughter Kerry,” she wrote. “It will be the greatest kindness for them to know that I am dead and where you found me – no matter how many years from now. Please find it in your heart to mail the contents of this bag to one of them.”
>The camp was less than two miles from the Appalachian trail. Adam wrote that walking south from the campsite, the dense forest became open woods with good visibility after 60-70 yards, and after another 25 minutes he found “a clear logging road” that led to lodging. In total the walk took about 30 minutes.

>> No.16045001
File: 129 KB, 994x1027, 009665.jpg [View same] [iqdb] [saucenao] [google]
16045001

>>16045000
https://www.centralmaine.com/2016/01/29/largay-died-in-a-sleeping-bag-inside-her-tent-report-says/

>> No.16045002

Not spaceflight shut the fuck up

>> No.16045004

>>16045002
it's a consequence of spaceflight, worldwide mid-band GSM cell coverage with normie cell phones. rather revolutionary stuff.

>> No.16045009
File: 38 KB, 655x560, 009666.jpg [View same] [iqdb] [saucenao] [google]
16045009

https://twitter.com/elonmusk/status/1762033996098379956

>> No.16045010

>>16045009
https://www.youtube.com/watch?v=3n7eNFj_9Vk

>> No.16045014

>>16044816
I do wonder how they'll fit in a launch abort system, since sticking a motor to a capsule on top won't be an option due to the header tank. Might have to go laterally and only then up and away, which seems like a fun engineering challenge to get to work both in flight and on the ground. The alternative would be something like separating the whole top half of Starship from the fuel tanks, which looks at first glance to be scary because it's introducing a seam into a previously-solid structure and the tile surface. Option C is to just not launch with humans aboard and to embark in space, Artemis style.

>> No.16045017

I don’t get it, why aren’t we getting pics from the moon? Were they really that incompetent as to mess up comms in 2024? No way, right?

>> No.16045019

>>16045017
The moon is in the way
Unironically

>> No.16045020

>>16045019
I won’t Google the engineering team and see a bunch of brown people will I? Definitely not a bunch of grad students?

>> No.16045022

I bet the IM bigwigs like Altemus and Crain are pretty fucking annoyed by the knowledge that Odysseus may very well have landed properly were it not for some chucklefuck wagie forgetting to flip a switch before launch.

>> No.16045027

>>16045020
>EagleCam is literally a student team
I need to renew my psychic license.

>> No.16045036

>>16045022
Even if it’s a diversity hire on the ops team who fucked up — the FACT IS they didn’t have a proper double-check process. Could you imagine if NASA or the armed forces made such a clownish India-tier mistake? And chef’s kiss was that it was NASA to bail out the mission from total failure. This is going to be used as pro-government/ pro-NASA ammo forever.

>> No.16045038

>>16044813
>>16044739
it would be VELY IMPLESSIVE

>> No.16045042

>>16045036
I suppose it could be used that way, but anyone who did should be reminded that if NASA/JPL made a lunar lander themselves in the present day it would likely cost at least 10x as much as any of these CLPS missions. My understanding is that the CLPS program is meant to help private industry build up some experience in developing lunar landers and give them government money to help them get through the early, amateurish fumbling stage and turn out a solid, reliable product eventually, and afterward NASA can just buy their services for much less than doing it all in-house. Time will tell, of course, how well this works with these small companies. Seems like the big dogs like SpaceX and BO have already poached most of the best aerospace engineers in the US.

>> No.16045048
File: 79 KB, 1080x1920, FB_IMG_1704031032999.jpg [View same] [iqdb] [saucenao] [google]
16045048

>>16044998
Can Starlink penetrate the forest canopy? It's all good if your area has coverage, but if you can't get a signal then its just as useless.

>> No.16045050

>>16045036
in the end it doesn't really matter, this means they have a problem in some procedures that need to be amended
if they do actually fix it, it is way better to iterate like this than use 10x the time and money to get it perfectly working the first time

>> No.16045051

>>16045048
see >>16044919

>> No.16045070
File: 203 KB, 1512x847, 4696532.jpg [View same] [iqdb] [saucenao] [google]
16045070

>>16044380
Starship sisters!! We are so back!!!
https://youtu.be/aGTyeGc-GRU

>> No.16045086

>>16044878
These could make starship flights to Mars a lot cheaper per person. Stack em like sardines in the SS, since they only need to be on board long enough to get to the cycler.

>> No.16045087

>>16045000
>>16045001
How can this even happen? If you're lost, use a compass to walk in one direction until you return to civilization.

>> No.16045092

>>16045048
How does the user upload data? Direct to satellite is a new thing, so they must be using some alternative.

Even direct to satellite is a problem wattage-wise, unless you had a big AESA antenna on your phone.

>> No.16045093

>>16044668
Intuitive Machines probably has people smarter and more knowledgeable than anyone here, yet they fucked up anyway. As with Astrobotics, JAXA, Ispace and others. Though one can argue it was due to special circumstances this time.

Of course it is physically possible to land a tall narrow lander that has a significant amount of mass high up. It just means the safety margins for error are narrower. SpaceX might be accepting tighter safety margins because they want to save money by re-purposing much of SS rather than building an entirely new lander from scratch, and they think this is will save far more money than they expect to lose by increasing the risk of failing and having to re-do the unmanned demonstration mission. So it can be simultaneously true that SS HLS is tippy while it also being a rational decision for SX to pursue it.

>> No.16045094
File: 260 KB, 1x1, GetAtt(2).pdf [View same] [iqdb] [saucenao] [google]
16045094

>>16045092
Normal 1900 MHz cellular band with unmodified phones. It's not meant to be efficient or high bandwidth.

>> No.16045098

>>16045093
>yet they fucked up anyway
Yes, by not removing a thingy before flight. That's quite a different thing than ZOMG LOOKS LIKE ITZ FINNA TIP OVAR.

>> No.16045105
File: 52 KB, 690x518, 00686eaKgy1hmf6rpt2qpj335s2dc7qc.jpg [View same] [iqdb] [saucenao] [google]
16045105

CASC's blue book projects 100 orbital launches by China in 2024, of which 70 by CASC
https://www.bjnews.com.cn/detail/1708932722129610.html

Space exploration:
* Queqiao 2 lunar relay
* Chang'e 6 Atkin basin sample return
* SVOM X-ray telescope

New CASC rockets:
* Long March 6C (boosterless variant of Long March 6A)
* Long March 12 (SAST's 3.8m diameter, quad-engine, single core rocket)

New liquid launch pads:
* Wenchang commercial pad
* Wenchang dedicated Long March 8 pad

>> No.16045106

>>16045098
They evidently fucked up using the software workaround too. Though, as said, one can argue it was due to special circumstances this time, they didn't have time to properly test the software patch

>> No.16045109

>>16045105
>New CASC rockets:
Also Long March 8G

>> No.16045119 [DELETED] 

>>16045010
https://litter.catbox.moe/b5jrmz.wav

>> No.16045122

>>16045010
https://litter.catbox.moe/5pgsj8.mp3

>> No.16045131

>>16044677
where is the spacex source for this?

>> No.16045138

>>16044917
>went from the gas powered model T in 1910 to electric powered lunar buggy in 1960s
technology moved so fast back then. we're only now seeing tech moving a bit faster than usual. the 60s-2010 were so slow. people used floppy disks for 30 years before moving to CDs.

>> No.16045142

>>16045009
option 5: managed democracy

>> No.16045143

>>16045105
say it with me "three hundred and fifty launches"

>> No.16045145
File: 147 KB, 1331x987, GHF0wQga4AAUWG_.jpg [View same] [iqdb] [saucenao] [google]
16045145

>> No.16045146

>>16045142
https://www.youtube.com/watch?v=S9STizATKjE

>> No.16045149
File: 126 KB, 603x720, a Taylor_Yow_EagleCam-01.jpg [View same] [iqdb] [saucenao] [google]
16045149

>>16045027
> Your EagleCam engineer is a literal sorority deb.

"Gooooo Thetas!"

>> No.16045152

>>16045138
Computers moved really fast 1960-2010. I think that was an important enabler for much progress in other fields. It enabled simulation and modeling that wasn't previously possible

>> No.16045161
File: 206 KB, 582x731, 1687427159625981.jpg [View same] [iqdb] [saucenao] [google]
16045161

SLIM lives
https://x.com/SLIM_JAXA/status/1762094730324902120?s=20

>> No.16045166
File: 61 KB, 400x300, 1692022556797010.png [View same] [iqdb] [saucenao] [google]
16045166

>Odysseus continues to communicate with flight controllers in Nova Control from the lunar surface. After understanding the end-to-end communication requirements, Odysseus sent images from the lunar surface of its vertical descent to its Malapert A landing site, representing the furthest south any vehicle has been able to land on the Moon and establish communication with ground controllers. 1/5 (26FEB2024 0745 CST)
https://x.com/Int_Machines/status/1762111937490378942?s=20

>> No.16045169

>>16045166
>Odysseus captured this image approximately 35 seconds after pitching over during its approach to the landing site. The camera is on the starboard aft-side of the lander in this phase. 2/5 (26FEB2024 0745 CST)
https://x.com/Int_Machines/status/1762111939142885816?s=20

>> No.16045170
File: 752 KB, 600x800, 1702214880564053.png [View same] [iqdb] [saucenao] [google]
16045170

>>16045169
Oops, forgot a photo.
>As part of Odysseus’ descent onto the lunar surface, Hazard Relative Navigation algorithms detected nine safe landing sites within the targeted south pole region, which is an area that contains permanently shadowed regions that may be rich in resources, including water ice that could be used for future propulsion and life support on the Moon. 3/5 (26FEB2024 0745 CST)

>> No.16045171

>>16045166
>>16045169
>picture dropped 30 minutes before the stock market opens
typical public company behavior, just like dropping bad news right after the market closes on friday

>> No.16045173
File: 10 KB, 262x82, Capture.jpg [View same] [iqdb] [saucenao] [google]
16045173

>>16045149
>tfw no giantess rocket scientist gf to step on you

captcha: sexo kilometers tall

>> No.16045174
File: 211 KB, 1500x843, GHREIQzXAAAtsFW.jpg [View same] [iqdb] [saucenao] [google]
16045174

>>16045170
>Images from NASA’s Lunar Reconnaissance Orbiter Camera team confirmed Odysseus completed its landing at 80.13°S and 1.44°E at a 2579 m elevation. After traveling more than 600,000 miles, Odysseus landed within 1.5 km of its intended Malapert A landing site, using a contingent laser range-finding system patched hours before landing. Image credit: NASA/Goddard/Arizona State University. https://lroc.asu.edu/posts/1360 4/5 (26FEB2024 0745 CST)

>> No.16045175

>>16045173
Imagine how much quicker you could build stuff with 15-20 ft tall pad workers

>> No.16045176
File: 239 KB, 1100x1100, im landing.webm [View same] [iqdb] [saucenao] [google]
16045176

>>16045174
>Flight controllers intend to collect data until the lander’s solar panels are no longer exposed to light. Based on Earth and Moon positioning, we believe flight controllers will continue to communicate with Odysseus until Tuesday morning. Image credit: NASA/Goddard/Arizona State University. 5/5 (26FEB2024 0745 CST)

>> No.16045177

>>16045175
>Fit like 5 of them in a Starship
>They get to Mars and assemble a base in a week

>> No.16045180

>>16045174
> completed its landing
> in a crashed sense of "completed"
> and missed its target

USA!

>> No.16045185
File: 155 KB, 1383x921, 009667.jpg [View same] [iqdb] [saucenao] [google]
16045185

https://twitter.com/stoke_space/status/1762114566580744613
>Upgraded stage two engine testing is off to a strong start.

https://pbs.twimg.com/media/GHRHrAaWEAAiQN8?format=jpg&name=4096x4096

>> No.16045189
File: 882 KB, 1298x716, nsf.png [View same] [iqdb] [saucenao] [google]
16045189

which car is NSF's?

>> No.16045194

>>16045166
>representing the furthest south any vehicle has been able to land on the Moon and establish communication with ground controllers
IM desperately trying to make this a success.
>>16045171
I wonder how long they've been sitting on all this for.

>> No.16045196

love from kazakhstan
I hate public companies so much it's unreal

>> No.16045198
File: 3 KB, 200x150, 1707252459251628.jpg [View same] [iqdb] [saucenao] [google]
16045198

>>16045189
None of your fookin business

>> No.16045199

>>16045174
>the nasa image was captured on the 24th but only released now right before the markets opened
hmmmmmmmmmmmmmmmmm

>> No.16045205
File: 215 KB, 1280x720, gfhjy67.jpg [View same] [iqdb] [saucenao] [google]
16045205

https://www.youtube.com/watch?v=nOIY4Kq0SHM
>Clues About SpaceX's Second Starship Launch Tower! | Starbase Update

>> No.16045211

>>16045092
the us government has been flying satellites for many years that can listen to normal cellphones, why can't starlink do it?

>> No.16045217
File: 896 KB, 807x597, Northrop Grunmann BOLEpng.png [View same] [iqdb] [saucenao] [google]
16045217

FIRST BOLE SEGMENT completed!

>> No.16045218

>>16045211
because those satellites have arrays larger than a football stadium

>> No.16045222

>>16045218
You want snooping to work even when the cellphone is close to its cell tower and using low power to transmit. Preferably from indoors too.

>> No.16045224
File: 79 KB, 580x463, shuttle giant comsat.jpg [View same] [iqdb] [saucenao] [google]
16045224

>> No.16045228
File: 94 KB, 940x748, MMU astronauts emergency rescue space shuttle.jpg [View same] [iqdb] [saucenao] [google]
16045228

>> No.16045258
File: 453 KB, 1390x1316, 1692916433859334.jpg [View same] [iqdb] [saucenao] [google]
16045258

That stupid lander landed in the worst possible location

>> No.16045260

>>16045217
I hope it blows up unironically. So much money sunk into this tech and it’s not advancing us one bit

>> No.16045261

>>16045258
*crashed

>> No.16045263

>>16045261
It's still in one piece and still works. I would call it a quite successful landing.

>> No.16045266
File: 125 KB, 357x572, sentinel.png [View same] [iqdb] [saucenao] [google]
16045266

>>16045260

>> No.16045267
File: 50 KB, 960x540, mgid_arc_imageassetref_shared.southpark.us.jpg [View same] [iqdb] [saucenao] [google]
16045267

>>16045228
looks like hes using his ballsack as a spacehopper

>> No.16045268

>>16045263
But the balls are not in the right orientation. How can you have a spiritual/cultural significant execution when you 100+ balls with names on the m are not pointed in the right direction?! It's insane to call it successful. You can't recharge the balls' energy when they're not pointed at the Sun. The names of all those wonderful people are now in some kind of multi-billion year purgatory of darkness; permanently belly-flopped - RAPED by someones failure to pay attention and flip the switch to turn the laser landing guidance system on. I can't stand this! I feel like I'm up there with all of those balls, forever.

>> No.16045269
File: 867 KB, 1818x1678, 1694554219850193.jpg [View same] [iqdb] [saucenao] [google]
16045269

They lost the technology...

>> No.16045271

>>16045269
those things didn't even have smart lander tech like the mars rovers. they literally just used altitude data from the radar to guide it during landing. no images etc.
I wonder if they just got lucky and never happened to come down on a boulder.

>> No.16045272
File: 64 KB, 762x598, Salvage.jpg [View same] [iqdb] [saucenao] [google]
16045272

>>16045268
Those balls are now legal to salvage, right?

>> No.16045279

>>16044767
Human training programs don't scale down well so the marginal cost is basically salary+spacesuit.

>> No.16045280
File: 63 KB, 960x730, CZ-10.jpg [View same] [iqdb] [saucenao] [google]
16045280

>>16045105
jfc they're making more rockets instead of focusing on the most important one

>> No.16045281

>>16045269
Landing by your previous lander to go check up on it and see how its doing is cool, we should do that more often. One day I hope astronauts brush the dust off Spirit/Opportunity's solar panels and dig them out from the sand.

>> No.16045282
File: 106 KB, 952x639, Pat Rawlings mars viking.jpg [View same] [iqdb] [saucenao] [google]
16045282

>>16045281

>> No.16045283

>>16045281
First Artemis mission with a rover should land as close as possible to Odysseus.

>> No.16045286

>>16045272
Someday - all these landing craft will have little museums around them. This one, too. And no one will know that it tipped over because Western culture was failing at the time and this failure was a perfect representation of that. The plaque will have the names of everyone who worked on the mission, and how it was so successful.

>> No.16045290
File: 64 KB, 473x781, Norman Rockwell apollo lem.jpg [View same] [iqdb] [saucenao] [google]
16045290

>>16045286
I think intact 20th C. landers and rovers will get preserved but not these early 21st C. wrecks

>> No.16045294

>>16045258
lol whoopsies!

>> No.16045296

Why is none of these files available anymore on NTRS?
https://www.orbiter-forum.com/threads/surveyor-lunar-rover.10411/

>> No.16045315

SLIM

LIVES

>> No.16045317

https://www.youtube.com/watch?v=Q6Fr-Whld6U

S28 getting tested

>> No.16045318

>>16045271
We lost many Surveyors on landing

>> No.16045320
File: 126 KB, 1918x1079, 009668.jpg [View same] [iqdb] [saucenao] [google]
16045320

>>16045317

>> No.16045321

> “As part of Odysseus’ descent onto the lunar surface, Intuitive Machines Hazard Relative Navigation algorithms detected nine safe landing sites within the targeted south pole region...

...and then we decided to crash somewhere unsafe. *beep boop*

>> No.16045326

>>16045290
>>16045286
there is something unbeleivably kino about how the lem left its descent stage on the moon. its unfortunate that future missions wont leave much apart from scattered science equipment.

>> No.16045329

>>16045176
> Odysseus landed wiithin a degraded one-kilometer diameter crater “where the local terrain is sloped at a sporty 12 degrees.

> picks a landing spot n a crater
> on a slope. 12 degrees is fairly steep
> then fell over and smashed into a boulder

Flat. You were supposed to land on FLAT!

>> No.16045331

>>16045087
>How can this even happen?
Panic is the usual answer, though sustaining an uninterrupted panic for over three weeks is an impressive feat, even for a woman.

>> No.16045334

Slim woke up after the lunar night. Will odie wake up after the night?

>> No.16045335
File: 3.66 MB, 620x380, 2024-02-26 17-42-10.gif [View same] [iqdb] [saucenao] [google]
16045335

>>16045329

>> No.16045336

>>16045331
pretty weird as she could have picked literally any direction and just kept walking and eventually something would have come up

>> No.16045339

>>16045329
> In the United States, maximum grade for Federally funded highways is specified in a design table with up to 6% generally allowed in mountainous areas and hilly urban areas with exceptions for up to 7% grades on mountainous roads with speed limits below 60 mph (95 km/h).

> "lands" on a 12% grade

>> No.16045345

>>16045329
>12 degrees
>>16045339
>12% grade

Not the same.
12 degrees is a 20% grade.

>> No.16045351

>>16044549
kinda amazing moon hoaxers never picked up on this. i've only seen them contend that the apollo reflectors were placed by unmanned probes, not that they're totally useless.

>> No.16045354

>>16045335
Should be used in a Viagra commercial.

>> No.16045358

>>16044549
holy shit don't let the moon landing deniers see this

>> No.16045360

>>16045296
NTRS changed their urls up years ago. you can find almost all old pdfs using archive.org

>> No.16045361

>>16044549
I ran the math. Doesn't add up. Everything in the sky is still flat.

>> No.16045365

>>16045296
because one senator found out about NTRS and FREAKED THE FUCK OUT ABOUT IT because china might read it, so NTRS underwent a purge.
https://nasawatch.com/itweb/nasa-technical-reports-server-mysteriously-taken-offline/
Fuck you Frank Wolf!

>> No.16045370

>>16045345
You are correct.

>> No.16045373

>>16045365
A US senator freaked out that China might read publicly available technical specs of a lander that was last relevant 50 years ago?

>> No.16045374

This is comedy https://twitter.com/StationCDRKelly/status/1761801998729433513

>> No.16045377

>>16045373
and a bunch of other old stuff too like performance of biplane propellers. The purge fucking sucks.

>> No.16045381

>>16045374
I think I understand why Slavs aren't considered white.

>> No.16045394

>>16045374
This shit has been cracking me up since yesterday lol
I don’t necessarily love rogozin but he’s the shitposter-in-chief and it’s funny watching him and his reddit ukulele flag enemies seethe at eachother kek

>> No.16045401
File: 107 KB, 1200x800, GHRZlgRbUAAXXNR.jpg [View same] [iqdb] [saucenao] [google]
16045401

見事越夜を果たした記念、流用で恐縮ですが
「もしもし? やっとつながった! すぐに観測再開を……はい?……まだ寝てろ??……ええと……」 などと言わせてみるテスト。

>> No.16045411

>>16045166
NSF forum comment on those astonishing HD images:

> The first might have been 40KB to downlink, the second, 7KB or less. They didn't just use low resolution (400x300), but also set the jpeg compression very high. It'd be a bit over 4 minutes to download the first pic, 45s to download the second.

Virtually nonexistent rate and signal strength.

>> No.16045423

>>16045374
lol he's mad

>> No.16045432

>>16045381
Pot calling the kettle black, but something like "monkey calling the gorilla a chimp".

>> No.16045435

>>16045401
See >>16044927

>> No.16045447

>>16045334
Official word is no
https://spacenews.com/intuitive-machines-expects-early-end-to-im-1-lunar-lander-mission/

>> No.16045460

>>16045334
No. IM-2 suffers the True Death on Tuesday.

>> No.16045464

>>16044924
and yet they STILL aren't going to tip it back upright with the RCS, are they

>> No.16045468 [DELETED] 

>>16045280
CZ-6C and CZ-12 are both SAST rockets. CZ-10 is a CALT rocket. So the projects use different resources to a large extent.

By the way, I don't think it's particularly important for CASC to hurry with the CZ-10. Many other companies in China are working on F9 clones. CASC is probably wise to focus on projects that are more schedule-safe, to bring more balance to the industry in terms of schedule predictability.

Schedule predictability is important for payload companies. If everyone focuses on new launchers that have a high risk of being delayed, there might be delays that ground payloads for years and cause enormous losses to payload companies and their customers. The risk might cause payload companies to hold back, meaning China might be in a situation of having a lot of launch capacity and not enough payloads to launch.

Since almost all new Chinese rockets under development are similar F9 clones, delays are not independent events. So just because China has 15 F9 cloning projects going in parallel, this does not reduce schedule risk.

Also, CZ-10 has a horrible payload mass fraction. It's a very suboptimal rocket, which I think is because it's a kludge solution that uses parts that weren't designed for it. I think CASC views CZ-10 mostly as a cheap-to-develop tech verification project with which they can get experience with booster recovery before they freeze the CZ-9 design, not as the future staple and workhorse on which the Chinese space program depends.

>> No.16045473 [DELETED] 

>>16045280
CZ-6C and CZ-12 are both SAST rockets. CZ-10 is a CALT rocket. So the projects use different resources to a large extent.

By the way, I don't think it's particularly important for CASC to hurry with the CZ-10. Many other companies in China are working on F9 clones. CASC is probably wise to focus on projects that are more schedule-safe, to bring more balance to the industry in terms of schedule predictability.

Schedule predictability is important for payload companies. If everyone focuses on new launchers that have a high risk of being delayed, there might be delays that ground payloads for years and cause enormous losses to payload companies and their customers. The risk might cause payload companies to hold back investment, so if there are few delays then China might get into a situation of having a lot of launch capacity but not enough payloads to launch.

Since almost all new Chinese rockets under development are similar F9 clones, delays are not independent events. So just because China has 15 F9 cloning projects going in parallel, this does not reduce schedule risk.

Also, CZ-10 has a horrible payload mass fraction. It's a very suboptimal rocket, which I think is because it's a kludge solution that uses parts that weren't designed for it. I think CASC views CZ-10 mostly as a cheap-to-develop tech verification project with which they can get experience with booster recovery before they freeze the CZ-9 design, not as the future staple and workhorse on which the Chinese space program depends.

>> No.16045474

>>16044549
So Nasa landed robots on the moon, so what?

>> No.16045485

>>16045280
CZ-6C and CZ-12 are both SAST rockets. CZ-10A is a CALT rocket. So the projects use different resources to a large extent.

By the way, I don't think it's particularly important for CASC to hurry with the CZ-10A. Many other companies in China are working on F9 clones. CASC is probably wise to focus on projects that are more schedule-safe, to bring more balance to the industry in terms of schedule predictability.

Schedule predictability is important for payload companies. If everyone focuses on new launchers that have a high risk of being delayed, there might be delays that ground payloads for years and cause enormous losses to payload companies and their customers. The risk might cause payload companies to hold back investment, so if there are few delays then China might get into a situation of having a lot of launch capacity but not enough payloads to launch.

Since almost all new Chinese rockets under development are similar F9 clones, delays are not independent events. So just because China has 15 F9 cloning projects going in parallel, this does not reduce schedule risk.

Also, CZ-10A has a horrible payload mass fraction. It's a very suboptimal rocket, which I think is because it's a kludge solution that uses parts that weren't designed for it. I think CASC views CZ-10A mostly as a cheap-to-develop tech verification project with which they can get experience with booster recovery before they freeze the CZ-9 design, not as the future staple and workhorse on which the Chinese space program depends.

CZ-10A is NET 2025Q4

>> No.16045487

China is awesome

>> No.16045493

>>16045411
How much payload data for the paying customers are they likely to have got? Enough?

>> No.16045494

https://payloadspace.com/lockheed-shows-off-its-new-speed/

they're finally starting to think like SpaceX

>> No.16045496

>>16045487
Every now and then they will illicit a bit of awe from me, yes. Usually just LM5 or crew launches though

>> No.16045499

>>16045485
Given that the CZ-10 is their new crew launcher the longer it takes to fly the farther out China's ambitions are pushed.

>> No.16045505

>>16045494
>Rather than relying on government contracts or predetermined mission objectives, the projects envisioned within Ignite are entirely funded by the organization.

Radical concept

>> No.16045512
File: 2.09 MB, 540x960, Hypergolic villager pillager.webm [View same] [iqdb] [saucenao] [google]
16045512

>>16045496
Everyone loses their shit when a big stage is tumbling out of control before reentry but I think it's funny.

>> No.16045521

>>16045512
So inefficient. The least they could do is try to use up those propellant residuals before crashing a stage into someone's house.

>> No.16045522

>>16045485
>Since almost all new Chinese rockets under development are similar F9 clones
*of the launchers that have realistic prospects of large scale use and affordability. Solids don't count.

>> No.16045531

>>16045499
Since they already have CZ-2F and Shenzhou, which are adequate for their space station needs, I think in terms of crewed missions it matters little how long CZ-10A is delayed. Right now they don't have anywhere else to send crew in LEO than their space station anyway.

The CZ-10 is for the crewed lunar missions, and is NET 2027. I suspect that CAST's Lanyue and Mengzhou probably wouldn't be ready for flight tests until around then anyway

>> No.16045542

What are the odds that China puts astronauts on the Moon before USA? Currently it looks like Artemis 3 will slip to 2028, and maybe even later.

>> No.16045547

>>16045542
the US put a man on the moon over 50 years ago, anon

>> No.16045551

>>16045542
80%

But they won't be able to keep up with the scale of Starship

>> No.16045552

>>16045547
That was the race between USA and USSR. Now we have a race between USA and China.

>> No.16045555

>>16045552
And yet we still put people on the moon before China, next question.

>> No.16045562

>>16045493
With that bandwidth over a couple of days? Customers got jack.

>> No.16045563

>>16045552
>>16045555
>>16045547
I guarantee that "who landed on the moon first?" will become one of those historical facts which is variable depending on where you live. Already 70% of russians think the OG moon landings were faked, and when china lands it will become a key tenant of their world order to claim that they are the true first country to the moon

>> No.16045564

>>16045555
What are the odds of Lanyue landing with people on the Moon before Starship?

>> No.16045566

>>16045542
https://twitter.com/globaltimesnews/status/1761257439369085251
>China’s Mengzhou spacecraft, the Lanyue moon lander, and the new-generation manned launch vehicle the Long March-10 have all entered preliminary development stage, and are proceeding smoothly. China aims to send taikonauts to the moon by 2030.

They could get there before we get back, but we'd really need to suffer some further delays to put them into a clear lead. The biggest advantage they've got is that their initial lunar exploration system is so conservative. They don't have to design and perfect any orbital refueling or reuse systems. The LM-10 uses the same tooling as the LM-5 and the YF-100 engine has plenty of flight time by this point. The capsule and the lander are the most complicated parts, but Mengzhou has been cooking for almost as long as Orion and Lanyue doesn't push for any huge capabilities beyond getting crew to the surface and back to LLO.

The other side of the coin is that the real moon race is about who can establish a permanent outpost first, and the various landers and launch vehicles under Artemis give America a pretty big advantage there. China will need something equivalent to the Long March 9 for anything more than flags-and-footprints and that still exists mostly as a PowerPoint demonstration.

>> No.16045570
File: 55 KB, 700x394, balls.jpg [View same] [iqdb] [saucenao] [google]
16045570

>>16045268
Are you saying... the balls are inert?

>> No.16045574

>>16045531
What was the point of this post my wumao friend, you didn't address what the anon said.

>the longer it takes to fly the farther out China's ambitions are pushed

>> No.16045577
File: 90 KB, 900x1042, 1700071314306852.png [View same] [iqdb] [saucenao] [google]
16045577

>went all-in on Intuitive Machines stock

>> No.16045583

>>16045281
They'd need to also swap out the batteries.

>> No.16045599

>>16045512
this is one thing I wish the USA did, but everyone is too big of a pussy

>> No.16045600

>>16045411
Return to text based communication and ASCII images

>> No.16045603

>>16045555
Yet you have no ability to defend your stake. It is China's for the taking

>> No.16045613

>>16045603
With what, a lander that is less capable than what America put on the Moon 50 years ago?

>> No.16045627

>>16045564
I would say pretty high because I have a strong feeling BO's Blue Moon will land the first group(s) of Artemis astronauts.
Starship HLS is a high risk very high reward system (if it works we can build the Artemis Basecamp easily) but it was the only system bidding at the time.

>>16045566
They're running into significant budget constraints too - remember their program is even more underfunded than Artemis.
This would be the most they've ever spent on space.

>> No.16045630
File: 155 KB, 902x486, Screen Shot 2024-02-26 at 9.38.53 PM.png [View same] [iqdb] [saucenao] [google]
16045630

We finally have the first picture from the surface. I'm starting to get really sick of you naysayers. Everything is find with the Lander. Just fine.

>> No.16045637

>>16045627
Artemis V, Blue's first landing, will happen after China's landing.

>> No.16045640

>>16045613
Is USA capable of defending your claimed lunar territory with your current capabilities? No

>> No.16045666

>>16045640
>claimed Lunar territories

Anyway, yes America is capable of pushing back China's nonexistant ability to claim the Moon.

>> No.16045694
File: 581 KB, 964x5810, CZ12_2.png [View same] [iqdb] [saucenao] [google]
16045694

Drawing of CZ-12, and comparison with Falcon 9

>> No.16045699

>>16045694
Rotate it so it doesn't turn into the dead sea scrolls

>> No.16045708
File: 49 KB, 86x468, cz-10.png [View same] [iqdb] [saucenao] [google]
16045708

>>16045531

This is not ideal for LEO as it's using the lunar rocket's (pretty heavy) second stage with 1 less engine as its upper stage hence bad mass fraction and TWR
They can probably optimize it like F9 v1.1 -> B5 though.
What's more important to them I guess is to have a reusable rocket that is crew rated asap.
YF-100 has actually failed twice now so it is below international standards (Merlin and RD-180) for crew.

>> No.16045715

>>16045708
>YF-100 has actually failed twice now
when did they fail? The CZ-5 and CZ-7A failures were both on the hydrolox stage, no?

>> No.16045730
File: 290 KB, 1004x1335, IMG_2984.jpg [View same] [iqdb] [saucenao] [google]
16045730

> The FAA has closed the mishap investigation into the second Starship test flight.

>> No.16045733

>>16045715
The CZ-7A might have been due to a YF-100 issue, but we've never got any official statement about why that launch failed. The CZ-5 Y2 launch failure was due to a turbopump issue with the YF-77 on the core stage.

>> No.16045739
File: 188 KB, 750x516, 0305FEA0-B916-4E39-A59D-0BABE98A55E7.jpg [View same] [iqdb] [saucenao] [google]
16045739

https://x.com/spacex/status/1762229838642082266

>> No.16045744

>>16045730
IFT 1 mishap investigation closure was on september 8, FAA finished their side of the licence authorisation on october 31, failure isn't as bad this time so Licence is no later than Mid-April.

>> No.16045746

what the hell?
on my phone, the Space X update page talks about what happened to the booster on flight 2, but on my PC, the website only shows the update prior to flight 2?

>> No.16045750

https://www.spacex.com/updates

>> No.16045751

>>16045739
Very unprofessional of SpaceX to respond on a social media platform.

>> No.16045753

>>16045750
>The most likely root cause for the booster RUD was determined to be filter blockage where liquid oxygen is supplied to the engines, leading to a loss of inlet pressure in engine oxidizer turbopumps that eventually resulted in one engine failing in a way that resulted in loss of the vehicle. SpaceX has since implemented hardware changes inside future booster oxidizer tanks to improve propellant filtration capabilities and refined operations to increase reliability.
Literally everyone BTFO

>> No.16045754

>>16045750
looks like they took it down right after they posted the update to fix a typo
On my phone, it still says February 23, 2024 not the 26th

>> No.16045755

>>16045751
hehe

>> No.16045756

>>16045753
basado

>> No.16045757

>>16045335
weeb lander bowing to the jap lander

>> No.16045758

>>16045753
all the water hammer simulations... for nothing...

>> No.16045760

>>16045757
YWNGTS

>> No.16045763

>>16045574
What use is a moon rocket with no moon lander or capsule?

I guess you could say the longer it takes to develop everything necessary, both rocket and payload, the further away China's space exploration ambitions are pushed. And this is true. But are they really the most important rocket/payloads for China to do in space? Commercial and military applications of space are very important, and aerospace resources are limited.

>> No.16045766

>>16045753
fluid hammer bros...

>> No.16045769

>>16045577
uh oh

>> No.16045774

sorry, Pedro left a box of bolts in the LOX tank

>> No.16045775

>The most likely root cause for the booster RUD was determined to be filter blockage where liquid oxygen is supplied to the engines, leading to a loss of inlet pressure in engine oxidizer turbopumps that eventually resulted in one engine failing in a way that resulted in loss of the vehicle. SpaceX has since implemented hardware changes inside future booster oxidizer tanks to improve propellant filtration capabilities and refined operations to increase reliability.

So all those new welds are a filter that stretches the width of the tank.

>> No.16045777
File: 266 KB, 1280x852, GHSToepWYAAQtva.jpg [View same] [iqdb] [saucenao] [google]
16045777

Are the Russians not training new cosmonauts anymore? It's always the same old cosmonauts being launched. These old men must be reaching accumulated days in space numbering 4 digits at this point.

>> No.16045782

>>16045753
> Raptor engine failed
Uhhh that's bad

>> No.16045792
File: 1.37 MB, 1920x1080, 1706415365452.png [View same] [iqdb] [saucenao] [google]
16045792

>>16045753
Going off of CSI Starbase's model of the plumbing, one of the LOX inlets got blocked by FOD or debris and led an engine to have an uncontained failure. It doesn't seem likely for multiple blockages have occurred since the LOX is pulled directly from the tanks.
Maybe water ice? Water ice is less dense than LOX and would've become an issue near the end of the flight.

>> No.16045795
File: 178 KB, 587x482, 1694742160261800.png [View same] [iqdb] [saucenao] [google]
16045795

Mishap investigation done
https://twitter.com/NASASpaceflight/status/1762237916120601028

>> No.16045796

>>16045760
>t. >>16045577

>> No.16045799
File: 97 KB, 1280x720, mooncarts.jpg [View same] [iqdb] [saucenao] [google]
16045799

>>16045566
>that still exists mostly as a PowerPoint demonstration.
They're testing components. It seems to me that YF-215 in 2023 was at approximately the development stage of Raptor in 2014. So they seem to be about on track for the stated schedule of a CZ-9 first launch in 2033, which is not long after a flag-and-footprint landing in 2029
https://spacenews.com/china-makes-progress-on-raptor-like-engines-for-super-heavy-rocket/

>China will need something equivalent to the Long March 9
They have an idea of assembling a base using pressurized moon carts (picrel). Could they perhaps be built light enough to be sent individually with CZ-10?

>> No.16045800

>>16045777
Their hair floats in zero gravity. We can't get enough of that. I think that's why they keep it long.

>> No.16045803
File: 361 KB, 3840x2160, 37c75ce2-e372-406e-8a1f-6aa622088501-original.jpg [View same] [iqdb] [saucenao] [google]
16045803

>>16045753
>filter blockage
>liquid oxygen
which filter? there's 103 distinct inlets for the 13 center engines.
doesn't seem likely something would affect that many engines at once

>> No.16045806

>>16045803
>103
13
>>16045792
yeah but that doesn't make sense. they say and one can see that many engines shut off due to reduced in let pressure. just one of them failed explosively.
where's would this common filter be? or was the tank literally full of 20000 ball bearings to clog them all?

>> No.16045807

>>16045753
this is bullshit. it was fluid hamer but they dont want to admit it because it would be an international scandal.

>> No.16045809

>>16045750
SpaceX really emphasised the move to electric TVC as an issue resolution for Starship, makes you think it was the hydraulics that blew up during the LOX dump.

>> No.16045812
File: 35 KB, 769x589, 3DF9B5DD-35C7-4F7D-BBD5-1FCB6C22A813.jpg [View same] [iqdb] [saucenao] [google]
16045812

>solves your FOD issue

>> No.16045818

>>16045812
?

>> No.16045820

https://ringwatchers.com/article/booster-prop-distribution
Here's the best resource about the center 13 LOX feed. Really don't understand. There is no common manifold.

>> No.16045821

>>16045753
muh hammer fluids...nooo

>> No.16045825
File: 960 KB, 1101x636, jeff and bill.png [View same] [iqdb] [saucenao] [google]
16045825

>>16045627
Ok Jeff, I'm going to need your team to build this thing in 2 years to beat the Chinese. Elon has failed us.

>> No.16045829

>>16045753
>>filter blockage
so does this mean we need to go back to building rockets in clean rooms?

>> No.16045831

>>16045799
The LM-10 should be able to handle an LM truck style lander, but the cargo wouldn't be much compared to Blue Moon and would be next to nothing when compared to Starship HLS. I haven't heard any estimates on the weight of the non-crasher half of Lanyue but the useful payload to the surface can't be much more than ten tons. There's also the issue of just how many LM-10s China can launch in a given period of time. I don't think Bejing would want to use the LM-10 as a base building rocket if it meant they'd have to skip that year's lunar landing.

>> No.16045832

>>16045825
I have a good feeling blue can get HLS done fast but there is no way Lockheed has cislunar transporter ready

>> No.16045833

>>16045812
they’re bringing back methane sweating btw

>> No.16045835

>>16045818
B9 blew up when a Raptor ingested methane ice.

>> No.16045839

>>16045014
>Option C is to just not launch with humans aboard and to embark in space, Artemis style
This is the only real option with the current design of Starship, maybe v2 will be wide and large enough for a launch escape system.

It's difficult to imagine a system large and robust enough to secure the really large passenger numbers that musk needs for a mars colony.

>> No.16045844

>>16045806
There could've been a thin layer of water ice on top of the LOX from contamination during fueling. Doesn't need a common filter if a bunch of water ice shards all got ingested by all the filters at once.

>> No.16045846

>>16045777
It’s pretty standard given the flight rate of Soyuz, don’t you think? The only russians going to space are doing so every crew rotation for the ISS. So not extremely often (especially now that everyone seems to be trying to keep humans in space for longer and longer durations. Both the US and Russia seem interested in this—which cuts down on the number of active astronauts you really need at one time)
All you need, really, is a reserve of ~20-30ish people who have been up once, twice, three times. Keep them on rotation. Every couple of years a few retire, so you bring in new people as-needed.

>> No.16045848

WAIT FAA CONCLUDED INVESTIGATION ON STARSHIP WHY ARENT YOU FAGS TALKING MORE ABOUT THIS??? WHY HAVE I NOT HEARD THIS YET WHAT THE FUCK

>> No.16045851

>>16045730
There was 1 (ONE) fucking post about this, biggest news on February and you FAGGOTS dont speak up more about it??? Im ashamed of you /sfg/

>> No.16045852

>>16045848
Literally just scroll up bozo

>> No.16045853

7 engines failed.
There was enough FOD in the tank to block 7 distinct filters?
Maybe I'm making a mistake.
Were they feeding from the landing tank? How does ullage gas get into that tank? Maybe there's the filter that got blocked.

>> No.16045856

>>16045853
>filters
What do you mean

>> No.16045858

>>16045844
Yeah okay that makes some sense.
If this was the last burn from the main tank and not from the landing tank already then it would have been nearing depletion.

>> No.16045859

>>16045853
The new filter spans the LOX tank, you can see the welds on >>16045812

>> No.16045860

>A leak in the aft section of the spacecraft that developed when the liquid oxygen vent was initiated resulted in a combustion event and subsequent fires that led to a loss of communication between the spacecraft’s flight computers. This resulted in a commanded shut down of all six engines prior to completion of the ascent burn, followed by the Autonomous Flight Safety System detecting a mission rule violation and activating the flight termination system, leading to vehicle breakup. The flight test’s conclusion came when the spacecraft was as at an altitude of ~150 km and a velocity of ~24,000 km/h, becoming the first Starship to reach outer space.

>becoming the first Starship to reach outer space.

Starship is officially a spacecraft now

>> No.16045861

>>16045860
Nope not till it reaches orbit, sorry. I’m absolutist on this. Kinda have to be, given how much I have bashed New Glenn at this point.

>> No.16045863

>>16045844
According to redditors quoting alleged insiders, the problem was CO2 and H2O ice from autogenous pressurization gasses. The gasses were "wetter" than expected and formed enough ice to clog the filters. These were posted last week before the SpaceX update so it's likely credible.

>> No.16045865

>>16045863
Wasn’t this a problem during the hop campaign?

>> No.16045866
File: 51 KB, 627x785, atmospheric layers.jpg [View same] [iqdb] [saucenao] [google]
16045866

>>16045861
>LEO/themosphere is space
Sorry, I’m absolutist on this

>> No.16045867
File: 349 KB, 556x616, GHS7Vj5XAAAIq64.png [View same] [iqdb] [saucenao] [google]
16045867

>onboard video

>> No.16045869

>>16045866
I don’t disagree on this now that I think about it

>> No.16045870
File: 35 KB, 604x235, file.png [View same] [iqdb] [saucenao] [google]
16045870

Well, in other news the FAA says Boeing sucks

>> No.16045871

>>16045867
>the LOX vent plumbing was leaky and dumped LOX into the hot engine bay.
neat

>> No.16045872

>>16045867
>internally called otf-2
worst version of the name ive heard yet. wasnt even orbital

>> No.16045873

Space starting at 600km is a bit of a stretch for me, but I agree that it's a bit silly to call 150km "space". It's still cope when we do it. It's at the very least not "outer space", isn't that past the heliopause anyway? Or is that the start of interstellar space?

>> No.16045874

>>16045872
FAA called it that, SpaceX were more autistic with their IFT

OFT is cooler anyways

>> No.16045877

>>16045865
I thought that was ullage collapse from sloshing?

>> No.16045878
File: 69 KB, 1082x1305, atmospheric layers 1.png [View same] [iqdb] [saucenao] [google]
16045878

>>16045869
Congratulations on becoming an exochad

>> No.16045883

>>16045863
Elon's best-part-is-no-part autism bites again if true. A dedicated methane/lox gas generator providing heat for an evaporator would've prevented this failure mode altogether.

>> No.16045887

>>16045883
He's still literally and exactly right about this. This might be the single thing he's most right about. If you never break something because you removed something essential, you haven't taken enough stuff off yet.

>> No.16045890
File: 355 KB, 628x525, n1 flight 3.png [View same] [iqdb] [saucenao] [google]
16045890

>all these failures even with modern technology and advanced computer simulations
Imagine what it was like trying to build the N1 back in the day lmao

>> No.16045891

>>16045883
Don't they have a heat exchanger for producing ullage on each engine?
That should isolate it from all combustion products.

>> No.16045893
File: 212 KB, 1280x757, 1696586167544467.jpg [View same] [iqdb] [saucenao] [google]
16045893

>france is considering sending troops to ukraine
https://www.reuters.com/world/europe/frances-macron-says-sending-troops-ukraine-cannot-be-ruled-out-2024-02-26/

obviously unlikely to happen, but since France is the major space power of the EU, what would the space battlefield look like in a war between Europe and Russia? i feel like Russia would push Europe's shit in when it comes to space.

>> No.16045894

>>16045891
according to the insider, they were using the LOX preburner tap-off for the LOX tank instead so the gas had CO2 and H2O in it.

>> No.16045896
File: 254 KB, 720x464, Olymp-K launched on Proton-M (2014).png [View same] [iqdb] [saucenao] [google]
16045896

>>16045893
Obviously Russia demolishes EU here (they straight up can't defend against Russian EW satellites) but the latter has America's help.

>> No.16045897

>>16045894
>according to the insider, they were using the LOX preburner tap-off
LMAO.
maybe they deleted the heat exchanger.

>> No.16045899

>>16045863
>Someone in the L2 forums pointed to issue out in January. They Best Parted too close to the sun and deleted the heat exchanger, dumping pre-burner exhaust straight into the lox tank. This works well for pressurization but there’s a tiny little issue.

>You dump hot CO, CO2 and H2O into the lox tank. What happens next? The gases condense, run down the walls of the tank and then form ice (and dry ice).

>This ice floats. Everything is perfect *until* the booster flipped over. Then all the turbopumps choked on slurry.

>> No.16045906

>>16045890
Honestly easier because despite their large sizes, both Saturn V and N1 were specifically designed to be overall-simple - with only strategic hurdles needed at any given time along the production process.
N1’s only problem was that it was being built by Russians. What’s worse; Russians under the USSR government. What a disaster, no wonder it failed!

>> No.16045907

>>16045894
>>16045899
This is so based actually. Best part is no part.

>> No.16045909

>>16045744
>Mid-April
AHAHAHHAHAHAAHHAHAHHA
Looks like another 2 launch year for you muskrats!

>> No.16045910

>>16045906
Untestable single-fire engines built by Russians

>> No.16045913

>>16045907
And there's not even an indication they reversed that decision.
Dumping water into your propellant tank to own the libs.

>> No.16045917

>>16045744
Hey faggot. Ever think that license time can drop from previous expectations? You should maybe go fuck yourself.

>> No.16045921

>>16045913
They added a filter to catch any ice.

Having to go back a step means you sufficiently Best Parted.

>> No.16045925

>>16045799
>surface habitats
i prefer the lavatube penetrator version

>> No.16045943

>>16045087
A lot of people don't pack a compass or a map or anything else. Or for that matter, they don't take a stock of their cardinal direction when they leave civilization behind and make a note of it, so that if they get lost, they have a direction to focus on to return to it.

And then as others have said, the overriding of logic caused by panic.

>> No.16045953

>>16045142
A managed democracy would lead to population collapse anywhere but Earth because of the extreme environmental hostility that exists without a stable local biosphere. The biggest weakness with democracy is that popularity matters more than ideas or merit. Trump won in 2016 despite having 0 political or governance experience, because he knew how to talk to the audience and worked the system in areas where his opponent, too arrogant to see her own weakness, ignored the constituents. Thereby ensuring that he locked in all core votes necessary for victory.

It's possible for a technocracy to eventually transition into a direct/managed democracy, but not vice-versa, as the probability of meritocratic decision making is unlikely to succeed due to inherent biases of humans bubbling up with our desire to be tribal no matter where we go.

>> No.16045967

>>16045913
when you have a high production rate they let you do it

>> No.16045970

>>16045943
Just about everyone who dies in the wilderness these days does so alone. Never hike alone.

Unless you're some crazy family who thinks living off the grid without any knowledge of how (actually happened)

>> No.16045974
File: 202 KB, 1280x2157, 1708893904878067.jpg [View same] [iqdb] [saucenao] [google]
16045974

>>16045970
Who am I supposed to hike with?

>> No.16045975

>>16045009
>homosexual Catholic's only visions of future governance are Islamic domination, robot domination, and vegan domination
The church has fallen

>> No.16045986

>>16045975
Kek

>> No.16045987

>>16045873
anything above 80 km is space

>> No.16045994

>>16045180
Could have been much worse, given the circumstances.

>> No.16045996
File: 749 KB, 958x918, 26e.png [View same] [iqdb] [saucenao] [google]
16045996

>>16045975
billions must psy

>> No.16046000

>>16045577
don't buy right after good news you tard
go all in on rocket lab the next time electron fails
t. non-investor

>> No.16046022

>>16045974
I went hiking with a girl from work and sucked her tits at the top

>> No.16046030

>>16045970
tfw no hiking gf

>> No.16046045
File: 3.97 MB, 422x270, haumea.gif [View same] [iqdb] [saucenao] [google]
16046045

rings

>> No.16046056

>>16045899
That doesn't sound very rapidly reusable if you have to clean your tanks of combustion products after every flight.

>> No.16046057
File: 9 KB, 489x413, Saturn's moon Methone, s.jpg [View same] [iqdb] [saucenao] [google]
16046057

why so schmooov?

>> No.16046058

>>16046045
That's cgi?

>> No.16046060

>>16044945
Perchlorates are literally the nothing burger of the century. Ever had a garden and over fertilized it? Boom you just made the ground toxic with perchlorates. Guess how you fix it? Washing it out with water.

>> No.16046066

>>16046057
Egg
>>16046058
Space Engine but yeah I guess cgi. Had to compress the file to post to 4cuck

>> No.16046071
File: 63 KB, 555x560, lunar motorbike.jpg [View same] [iqdb] [saucenao] [google]
16046071

How would you change bikes for a huge low g shirtsleeve environment?

>> No.16046077
File: 40 KB, 611x448, twr isp 2.jpg [View same] [iqdb] [saucenao] [google]
16046077

>> No.16046081
File: 82 KB, 828x551, Firing Room 1 at successful launch of shuttle STS-1, April 12, 1981.jpg [View same] [iqdb] [saucenao] [google]
16046081

>> No.16046094

>>16046071
Tune up the suspension but that's about it. Bikes are simple things. Even for lunar ops an electric dirtbike only needs different wheels and suspension settings.

>> No.16046098

There’s so much SpaceX cock-sucking it makes me super suspicious of any good news or hype re Starship. The company doesn’t seem to be suffering under a terrible competency crisis as most American tech companies are — but it’s seems out-of-order how MUCH failures they suffer with core tech. Yes Elon arrived on the scene at just the right time to exploit the battery revolution and yes he was able to execute on major government contracts and thereby secure the funding needed to grab up the best orbital bands — but it needn’t have been SpaceX it could have been anyone who grabbed that business. SpaceX was competent enough to successfully execute on that government work which in the end of that is all that matters — but I feel like soiface propaganda constantly bombarding me about how awesome Starship is going to be when all I see are failures. Can someone explain?

>> No.16046100
File: 752 KB, 1080x1674, Screenshot_20240227-114625-528.png [View same] [iqdb] [saucenao] [google]
16046100

>>16045374
For reference

>> No.16046107

>>16046098
Concern trolling.

>> No.16046113

>>16044872
more void/air space

>> No.16046122
File: 110 KB, 1087x521, spin launch rocket g load.jpg [View same] [iqdb] [saucenao] [google]
16046122

Any news on Spinlaunch?

>> No.16046124

>>16045803
It was one engine that exploded and that cascaded

>> No.16046127

>>16044770
the real red pill is hydrophobic ceramics. TPS absorbing water was a big part of the problem the shuttle had. It needed a weird fucking coating or else it'd absorb water like a sponge. Hydrophobic ceramics might not have this problem.
https://www.nature.com/articles/nmat3545

>> No.16046128

>>16045829
Need to purge the tanks and lines better, thats it

>> No.16046131

>>16046128
anon they're literally dumping preburner tapoff into the tanks to pressurize them during flight, that's going to cause a lot of ice to freeze out and clog things if the filters aren't up to task

>> No.16046134

>>16045883
Thats why you test
A better filtering syatem might be cheaper and lighter than a heat exchanger

>> No.16046136

>>16046131
so it wasn't all the bird crap, bugs, and loose metal clogging up the filters?
>>dumping preburner tapoff into the tanks to pressurize them during flight
that sounds retarded, but what do I know

>> No.16046138

>>16046056
Just flush it nigga, how hard can that be

>> No.16046140

>>16046131
fucking source?

>> No.16046144

Realistically how long will it take for BO, Relativity, Rocket Lab, ANYBODY to get to SpaceXs cadence?

>> No.16046147

>17 corrective actions
What are the 17 corrective actions?

>> No.16046151

>>16046131
Just make better filters

>> No.16046156

>>16046147
17 payoffs

>> No.16046158

>>16046098
when i make this kind of bait, i write considerably less. and instead of SpaceX write it as "space-x"

>> No.16046159

>>16046122
Right now it sounds like they're stuck trying to finding a good site for their orbital launch system. They were thinking about Hawaii but that went about as well as you'd expect. Now they're looking at some spots in Alaska and Australia.

>> No.16046163

>>16046098
it's simple: you're retarded.

>> No.16046171

>>16046098
its due to hardware rich iterative development and questioning every requirement instead of just doing something because it is supposed be how you do it
all in all it seems to result in a development programme that is much quicker and cheaper with better ultimate results
you could have the "failures" in simulation as an alternative but then you get BO or oldspace or SLS

>> No.16046179

>>16045777
Tracy Caldwell Dyson looks uncomfortably like Elon Musk in this picture. Uncanny

>> No.16046207

>>16046113
Does it still perform better at that point?

>>16046138
Oh I don't doubt it's not too hard, but it's definitely a hindrance to the whole just fill it back up and launch again bro mindset.

>>16046147
Take a look at the report your company wrote Elon, they're in there.

>> No.16046214

Do we know when the next varda launch is? Transporter-11 isn’t until July which is a hell of a ways away

>> No.16046217

>>16046081
Makes me want to re-watch the Apollo 11 docu from 2019. That movie is so kino

>> No.16046218

>>16046207
yes, air space doesn't affect temperature tolerance

>> No.16046219

>>16046214
do we even know how the first one went? they just got it back, have they published that it was successful yet?

>> No.16046222
File: 585 KB, 1200x675, untoppleable.png [View same] [iqdb] [saucenao] [google]
16046222

>>16044506
they improved the legs to reduce toppleage

>> No.16046224
File: 456 KB, 1152x2048, GHT_QBZXQAAdgsb.jpg [View same] [iqdb] [saucenao] [google]
16046224

https://twitter.com/PointOrView/status/1762314012128104589/
>Prashanth Nair
>Angad Prathap
>Ajit Krishnan
>and Chauhan
Sirs, we have our astronauts

>> No.16046228
File: 88 KB, 660x662, 009669.jpg [View same] [iqdb] [saucenao] [google]
16046228

https://twitter.com/andrewmccalip/status/1761905126917423389
>12 years ago I interned at SpaceX with one of the smartest guys I had ever met. We worked nonstop nearly every day that summer, it was a magical place with rockets and the vibes of 1960s NASA. 115 engineers interns living together at Oakwood, many of whom now run the new space industry. Our paths branched when I ended up turning Juncosa down so that I could go back to Texas, get married, and start a business. Entrepreneurialism was life-changing journey in my 20s, and I knew I wanted to do round 2 in a big way. '
>Fast-forward 9 years, and a fast talking guy with mismatched shoes (Delian) is shouting about the expanding the economic bounds of mankind and Atoms not Bits. SpaceX pioneered access to space, now what do we do with that??? Can we assemble a team of seasoned engineers to pull off an insane timeline, going from 0-1 in two years?
>The next three years were an absolute rollercoaster. One day we'll assemble all the footage and tell the story. Easily the hardest thing that any of us had ever done. In the end, success is largely determined by sheer willpower of the team. Yeah, you can assemble a smart group, but ultimately it's grit and willpower that gets you over the finish line. Never seen a team like them, we definitely got lightning in a bottle.
>The tremendous success of this first mission means that we can focus on the next stage. Relentless high cadence customer focused operations. To quote Elon, "It will be successful, ironically, when it becomes boring".

>> No.16046230

>>16044776
>dream ship
>monopolize the moon
neat!

>> No.16046231
File: 315 KB, 1385x1039, GHOLOvzbsAAjsE5.jpg [View same] [iqdb] [saucenao] [google]
16046231

>>16046228

>> No.16046234

>>16044996
>logarithm percentages
>4 data points, at least one is made up
>no visible pattern or reason to make a graph in the first place
I kneel

>> No.16046239

>>16046234
its a point prediction with a few historical data points to put it into context

>> No.16046247

>>16046234
Ark's relationship with reality is even more tenuous than the average analyst's, pay them no attention. Elon only replies to them because they relentlessly hype his companies.

>> No.16046253
File: 232 KB, 640x426, whalers-on-the-moon.png [View same] [iqdb] [saucenao] [google]
16046253

>>16046222
TRIPS IS TRUTH! WE SHOULD HARPOON THE MOON!

>> No.16046279

>>16045009
>Martian technocracy
Does that mean mars ruling over earth?

>> No.16046280

>>16045566
>the real moon race is about who can establish a permanent outpost first
This is never happening lmao

>> No.16046290
File: 185 KB, 1024x1024, _ea81f8b7-9bd7-4039-a64b-f94807685177.jpg [View same] [iqdb] [saucenao] [google]
16046290

>>16046279
Mars for Martians

>> No.16046299

>>16046290
Kill yourself

>> No.16046300
File: 31 KB, 640x480, ec293f3d-3ecd-47cf-9ad5-477eba5dca65_screenshot.jpg [View same] [iqdb] [saucenao] [google]
16046300

>>16046253
That's not how it happened at all! They were just using whaling as a metaphor for beating their wives.

>> No.16046306

Elon Said OFT-3 Flies In March

>> No.16046320

>>16046306
8th of March NET

>> No.16046323

>>16046320
more like NLT

>> No.16046329

>>16046323
that doesn't make any sense

>> No.16046369
File: 40 KB, 681x681, ingenuity-1.jpg [View same] [iqdb] [saucenao] [google]
16046369

https://arstechnica.com/space/2024/02/final-images-of-ingenuity-reveal-an-entire-blade-broke-off-the-helicopter/
>Final images of Ingenuity reveal an entire blade broke off the helicopter
>This happened last month. On January 6, Ingenuity flew 40 feet (12 meters) skyward but then made an unplanned early landing after just 35 seconds. Twelve days later, operators intended to troubleshoot the vehicle with a quick up-and-down test. Data from the vehicle indicated that it ascended to 40 feet again during this test, but then communications were ominously lost at the end of the flight.

>> No.16046371
File: 109 KB, 1208x1208, ingenuity-2.jpg [View same] [iqdb] [saucenao] [google]
16046371

>>16046369
>A broken blade in an ancient channel on Mars.
>The new images are remarkable in that they reveal Ingenuity more clearly than before and show that one rotor blade was completely broken off. Additional sleuthing revealed that this blade lay about 15 meters away from Ingenuity on the red Martian sands, apparently winging away from the helicopter prior to or during a landing of the vehicle on its final flight last month.

>> No.16046374
File: 112 KB, 933x820, 009670.jpg [View same] [iqdb] [saucenao] [google]
16046374

>>16045166
https://arstechnica.com/space/2024/02/nasa-found-the-private-lander-on-the-moon-but-its-lifetime-is-running-short/
>In an update posted on Monday morning, the company that built the spacecraft, Intuitive Machines, said, "[W]e believe flight controllers will continue to communicate with Odysseus until Tuesday morning." This is because the lander, which is tipped over on its side, will only be able to collect solar energy for a limited period of time.
>Originally, the company had hoped to operate its privately developed lunar lander on the surface for a week or longer. But now, that will no longer be possible due to the limited ability of Odysseus to gather solar energy and remain powered on. As the Sun dips closer to the horizon, and with the two-week-long lunar night coming, the spacecraft will, effectively, freeze to death.

>> No.16046380
File: 101 KB, 965x790, 009671.jpg [View same] [iqdb] [saucenao] [google]
16046380

https://www.cnbc.com/2024/02/26/faa-closes-starship-investigation-spacex-seeks-next-launch-license.html
>The 17 corrective actions following the second Starship flight also represent a marked improvement from the first, which required 63 corrective actions before the rocket launched again.
>Musk said in a social media discussion last week that he expects the company to be ready to launch the third Starship test flight as soon as mid-March, although the SpaceX CEO also said, shortly after the November launch, that the third flight’s rocket would be “ready to fly in three to four weeks.”

>> No.16046382
File: 95 KB, 924x844, 009672.jpg [View same] [iqdb] [saucenao] [google]
16046382

https://arstechnica.com/space/2024/02/faa-closes-starship-inquiry-and-spacex-details-causes-of-november-accidents/
>SpaceX has four Starships in complete, or nearly complete, build stages. Should the next flight go smoothly, the company could begin to launch the world's largest rocket on a more frequent basis.

>> No.16046386

>>16045974
Join a meetup group and go hiking with them you autistic degenerate.

>> No.16046389
File: 133 KB, 1064x760, 009673.jpg [View same] [iqdb] [saucenao] [google]
16046389

https://www.thespacereview.com/article/4749/1

>> No.16046391

>>16046098

Explain why nobody else but SpaceX has managed to propulsively land their boosters in the 9 years since they achieved their first landing and 11 years since they started their grasshopper tests. Also explain why everybody's earliest reusable booster design and implementation plans lead out to 2030 and no earlier. Blue Origin says they intend to land New Glenn on first flight, it's not impossible but would be surprised if they could land something that massive without having flown it even once.

>> No.16046397
File: 215 KB, 1059x606, 009674.jpg [View same] [iqdb] [saucenao] [google]
16046397

>>16046389

>> No.16046398

>>16046369
>>16046371
I don't think it broke during landing or even seconds before landing, but at its height. It probably took damage in the first flight, and because the blades have to spin at such high rpms to generate enough lift under Mars' 1% dense atmosphere, during ascent of second flight, it sheared off and went the 15 meters while the drone had its power cut as a result of catastrophic failure and simply just fell back to the sand, and given the 38% Earth gravity environment and the sand itself being soft, the fall was surprisingly gentle despite the height.

>> No.16046403

>>16046389
>>16046397
Partial success, not a complete failure. For a startup to land on the moon without total destruction of the probe is a bit like SpaceX reaching orbit with the Falcon 1 with the very last booster they had and no money in the bank. Unfortunately, I don't think there's another 2010-2012 NASA that's got a CRS equivalent contract lined up to save Intuitive Machines, especially with the way their stock performance is going. So unless they have enough money in the bank for another probe, they'd be up for either a buyout by someone bigger or would likely have to give up a lot of equity that's retained internally to raise enough money to avoid going belly up.

>> No.16046406
File: 109 KB, 398x275, what2.png [View same] [iqdb] [saucenao] [google]
16046406

>>16046098
Compare [accomplishments of Spacex] to [accomplishments of any other aerospace company]

>> No.16046408

>>16046403
IM-2 and IM-3 have already been contracted I think
IM-2 will launch in fall and IM-3 next year

https://www.nasa.gov/event/intuitive-machines-clps-flight-im-2/
https://en.wikipedia.org/wiki/Intuitive_Machines_Nova-C#IM-2_mission

>> No.16046414
File: 89 KB, 2286x450, Soyuz.png [View same] [iqdb] [saucenao] [google]
16046414

>>16045777
This used to be the case but kinda isnt anymore. there was a period before 2020 where they were sending up guys for their 4th or 5th flight alongside NASA and ESA astronauts. only room for 3 on the soyuz I guess so no room for the rookies.
But since 2020 they've had about 7 new russian cosmonauts going up.
Ivan, Sergey, Pyotr, Denis, Sergey, Dmitry and Nikolai
About an average of 2 new cosmonauts per year. not counting the tv director/actress who went up on Soyuz MS-19

>> No.16046423

>>16046107
Yep, but other retards still fed (You)s to that fag after you posted this. /sfg/ is retarded

>> No.16046438
File: 47 KB, 689x624, 009676.jpg [View same] [iqdb] [saucenao] [google]
16046438

https://twitter.com/michaelnicollsx/status/1762149124949049627

>> No.16046458

>>16046438
F9 has a tight bussy

>> No.16046525
File: 57 KB, 1179x239, IMG_3710.jpg [View same] [iqdb] [saucenao] [google]
16046525

Staging

>>16046524
>>16046524
>>16046524
>>16046524
>>16046524

>> No.16046552

>>16046406
stupid frogposter

>> No.16046556

>>16046060
also worms love to eat them

>> No.16046598

>>16044549
The reflectors are damaged by dust but it's not like they don't work. That paper is bunk.

https://tmurphy.physics.ucsd.edu/papers/Icarus-208-31.pdf

>> No.16046729

>>16044506
SpaceX can land boosters. IM can't land jack shit.

>> No.16046757

>>16046369
Tip culture s m h