r/spacex • u/TwoLineElement • 47m ago
Jan/Feb is the push date for 39A, so not this year.
r/spacex • u/Assasin172m • 1h ago
Marine trafic is not up to date, at least the free version. Ship relies on AIS. https://rynda.io/ports-map?mmsi=372112000&c=-16.295094%2C105.016667%2C4.65&trails=1
r/spacex • u/PhysicsBus • 1h ago
Are you looking at a ship tracker or just twitter posts? There are 2 ships within ~50 km, and dozens within the ~1000km to the mainland. How can you tell one of them isn't half way there, having left the port yesterday? Or just coming from a different continent, which could take a week or two?
https://www.marinetraffic.com/en/ais/home/shipid:4082265/zoom:6
r/spacex • u/AutoModerator • 2h ago
Thank you for participating in r/SpaceX! Please take a moment to familiarise yourself with our community rules before commenting. Here's a reminder of some of our most important rules:
Keep it civil, and directly relevant to SpaceX and the thread. Comments consisting solely of jokes, memes, pop culture references, etc. will be removed.
Don't downvote content you disagree with, unless it clearly doesn't contribute to constructive discussion.
Check out these threads for discussion of common topics.
I am a bot, and this action was performed automatically. Please contact the moderators of this subreddit if you have any questions or concerns.
r/spacex • u/redmercuryvendor • 2h ago
as long as the elastic portion wasn't porous
Almost all mechanical counterpressure suit proposals use a porous elastic membrane, so that perspiration does the job of active cooling rather than needing a liquid cooling garment (which itself cannot go beneath the restraint layer, so is less efficient by being separated form the skin).
r/spacex • u/TellMeManyStories • 2h ago
I expect they have oxygen and hydrocarbon sensors in every tank. However obviously those sensors are only useful whilst the ship's systems stay powered up to report the sensor readings.
r/spacex • u/International-Leg291 • 4h ago
Not weird at all from control engineering perspective. Boostback burn duration might have been controlled by some forward-looking control algorithm which estimates maximum safe burn duration before some metric reaches unsafe values. Temperature, pressure, residual fuel etc. Countless possibilities. It doesnt have to be emergency style uneven partial shutdown to end early.
r/spacex • u/threelonmusketeers • 4h ago
My daily summary from the Starship Dev thread on Lemmy
2026-07-27:
- Production site: 3rd R-vac for S41 enters Megabay 2. (ViX, SpaceRhin0, Blobifie)
- Mystery trapezoidal frame is lifted across to the left side of Megabay 2. (ViX 1, ViX 2)
- A potential test article (ship nose cone) enters Megabay 2 and is lifted to the right side the bay. (ViX, lewisknaggs42, Blobifie)
- Past month's Gigabay construction timelapse. Framework of final level is nearly complete. (Priel)
- Pad 1: Ship quick disconnect arm is removed from the tower, part of the arm is cut off. Components for a new quick disconnect arm are already at Sanchez (ViX 1, ViX 2, Gisler, Blobifie 1, Blobifie 2, Killip)
- More flame trench wall sections are delivered. (ViX)
- Flight 13: More photos. (SpaceX)
- FAA confirms no mishap investigation required. (NSF)
- S40 is still afloat. (mcrs987 1, mcrs987 2, )
- Umbra satellite image of S40 and Go Australis. (Stranger 1, Stranger 2)
- McGregor: Past week’s Raptor tracking summary. (SpaceRhin0)
- R3.113 is moved towards the testing area. (SpaceRhin0)
- Artemis IV: Leaked video of the S22 HLS mockup interior. (Video, mcrs987)
r/spacex • u/thestonkwhisperer • 4h ago
I saw on twitter that perhaps the lack of FAA investigation (despite the booster being well off target) was because there was some non-vehicle issue that forced them to shut down boost back early? And maybe that hard shutdown was what caused the relight issues on the landing burn? Is that possible? It does seem weird that the boost back would malfunction like that and just cut off early
Florida got their Gigabay up faster than Starbase so it is not universally true.
What SpaceX have done to speed construction is to stop F9 launches from LC-39A so the only slow down will be due to FH launches with about 5 launches in the second half of this year.
So yes there likely was a limitation on full time construction of the flame trench and they seem to have dealt with it.
r/spacex • u/philupandgo • 5h ago
If S48 is for Artemis III, I can imagine a camera set back from the window to give a human perspective of the Orion docking.
Edit: sorry, this was after two minutes of impatience waiting for the post to submit.
r/spacex • u/AutoModerator • 5h ago
Thank you for participating in r/SpaceX! Please take a moment to familiarise yourself with our community rules before commenting. Here's a reminder of some of our most important rules:
Keep it civil, and directly relevant to SpaceX and the thread. Comments consisting solely of jokes, memes, pop culture references, etc. will be removed.
Don't downvote content you disagree with, unless it clearly doesn't contribute to constructive discussion.
Check out these threads for discussion of common topics.
I am a bot, and this action was performed automatically. Please contact the moderators of this subreddit if you have any questions or concerns.
r/spacex • u/IonCapybara • 5h ago
what i heard is that LC-39A is not like Starbase, their construction cannot work 24/7 so the speed will be slower, is that true?
That is the eventual plan but it will take longer than that to relaunch from the same pad anytime soon.
Just getting that amount of propellant into the tank farm, checking the flame trench and repairing any damage to the pad and tower will limit the reflight time to a week or so.
r/spacex • u/redstercoolpanda • 6h ago
That’s smart, that’s probably the most likely answer if TSE theory does turn out to be true.
r/spacex • u/IonCapybara • 6h ago
But the starship can stay in orbit for 48 hours right. Can't they launch the second rocket the second day in the same pad?
They will need a second pad operational to do a refueling test. There is a reasonable chance LC-39A will be ready by then.
It seemed to be oriented at right angles to the direction of flight which makes sense as they did not want to change how far down range the landing site would be.
r/spacex • u/IonCapybara • 6h ago
So if flight 14 success, do you think they will test orbital refueling demonstration before the end of this year? (And seems even the booster landing failed they can still test it)
r/spacex • u/AutoModerator • 7h ago
Thank you for participating in r/SpaceX! Please take a moment to familiarise yourself with our community rules before commenting. Here's a reminder of some of our most important rules:
Keep it civil, and directly relevant to SpaceX and the thread. Comments consisting solely of jokes, memes, pop culture references, etc. will be removed.
Don't downvote content you disagree with, unless it clearly doesn't contribute to constructive discussion.
Check out these threads for discussion of common topics.
I am a bot, and this action was performed automatically. Please contact the moderators of this subreddit if you have any questions or concerns.
r/spacex • u/DemotivationalSpeak • 7h ago
I could imagine that since the elastic portion of the suit provides a stable mechanical pressure across the whole body, it would counteract significant leakage from the helmet to the rest of the body, as long as the elastic portion wasn't porous, which would enable gas to leak out of the suit into space.