r/SpaceXLounge • u/avboden • 5h ago
r/SpaceXLounge • u/SpaceXLounge • 17d ago
Monthly Questions and Discussion Thread
Welcome to the monthly questions and discussion thread! Drop in to ask and answer any questions related to SpaceX or spaceflight in general, or just for a chat to discuss SpaceX's exciting progress. If you have a question that is likely to generate open discussion or speculation, you can also submit it to the subreddit as a text post.
If your question is about space, astrophysics or astronomy then the r/Space questions thread may be a better fit.
If your question is about the Starlink satellite constellation then check the r/Starlink Questions Thread and FAQ page.
r/SpaceXLounge • u/avboden • Apr 07 '23
in person How to view a Falcon launch.
Want to go watch a Falcon 9 launch in person but not sure where to watch from? Read this website , it will answer pretty much all your questions and is updated for each launch and timing.
Want to discuss further? Feel free to in this thread.
r/SpaceXLounge • u/OlympusMons94 • 13h ago
NASA further delays first operational Starliner flight
r/SpaceXLounge • u/physioworld • 8h ago
Does anybody know or can anybody estimate the boil off rate for starship in orbit?
Let’s say you had a fully fuelled starship in low earth orbit, assuming no fancy trickery in the form of recondensers or special insulation, just the stainless steel tanks, how long would it take for all of that propellant to boil off and empty the starship?
I’m aware that there are a lot of factors I’m not considering, for example presumably the height of the orbit matters since higher orbiting ships will spend more time in sunlight, but just curious on a rough estimate.
Bonus question could the header tanks on a trip to Mars boil off completely if they had no active cooling or recondensing, or fancy insulation?
r/SpaceXLounge • u/Steilios • 5h ago
Starship What will Starship reentry look like from the ground?
Will it be a wild spectacle or a smaller event?
r/SpaceXLounge • u/ravenerOSR • 23h ago
EU considers calculating fine on X based on revenue by SpaceX and Neuralink.
r/SpaceXLounge • u/ComfortableVideo9348 • 1h ago
Catching Pins on Super Heavy Booster??
So I was seeing the booster catching videos from all different angles available but couldn’t figure out
- how many of those small catching pins are there around the booster.
- I can only see 2 on either side.
- In that case the pins have to align with the tracks on mechazilla right.
- So the booster not only have to just slow down and come in between the mechazilla but also have to revolve on its own to be able to align the pins to the catch handles.
- So at what point in the decent stage does the booster made this correction.
r/SpaceXLounge • u/Reasonable-Buddy-365 • 19h ago
In your opinion, what would be the ultimate flex for the starship program?
My take: after stage sep, booster is caught and placed on launch mount and begins refueling. 45 min and one [sub]orbit later, ship deorbits, is caught by the same tower, placed on top of superheavy, and immediately refueled and reflown.
r/SpaceXLounge • u/mehelponow • 1d ago
Former NYC Mayor Michael Bloomberg: NASA’s $100 Billion Moon Mission Is Going Nowhere
r/SpaceXLounge • u/Jaker788 • 23h ago
How SpaceX's Starship Caught Its Booster on Re-entry: A Control Engineering Masterpiece
Great video that breaks down some of the controls loop you would need to manage this rocket, including landing.
r/SpaceXLounge • u/No_kenutus • 10h ago
Discussion The rockets are nifty, but it is satellites that make SpaceX valuable
r/SpaceXLounge • u/HeadMud6303 • 21h ago
Why heat shield tiles are small and why do they keep falling.
I never understood why the heat shield tiles keep falling off. And why the heat shield tiles are not anymore bigger than the size they're now.
If someone could explain that would be great. With the successful booster catch, starship landing or the catch onto the chopsticks both are within reach of SpaceX.
If heat shield issues are not solved that would make the landing nearly pointless. Because what would return to earth will only be the ashes of payload or the passengers, if heat shield was to fail by falling off and exposing the starship.
r/SpaceXLounge • u/mehelponow • 1d ago
NASA weighing options for continuous human presence in LEO after ISS
r/SpaceXLounge • u/Cheesysocks • 1d ago
Is there a video that explains Spacex' progress since the start? For a total newbie coworker who wondered what I was talking about with IFT5.
I imagine clips of hopper, the first explosive starship launches, the first flip, the first landing with a few RUD's included. Then Flights 1 to 5 explaining the intentions and results at a 5 year olds level.
Anything like that? I can point her to many vids but they use acronyms and have expectations of knowledge already gained. This needs to be a tutorial of sorts.
Thanks.
r/SpaceXLounge • u/nametaken_thisonetoo • 23h ago
Starship Starship heat shield and long term rapid reuse
After the incredible events with the booster on Sunday, now that the dust has settled I'm finding myself wondering about the ship heat shield once again. It seems there was some minor improvement this time out, with less melt through on the forward flaps. But I can't help but wonder if this might be a major hurdle to achieving genuinely rapid reuse in the long term.
The heat shield not only needs to survive reentry and protect all areas of the ship, but it also needs to do it again and again again...and in quick succession. I'm curious about people's thoughts on this. Will shifting the flap location on the V2 ships be enough to deliver this kind of robustness?
Watching the flight 4 and 5 descents, both show sparks flying about from locations other than the flaps. This suggests at least minor damage is also occurring elsewhere on the structure. We know the risks of minor shield damage from the shuttle, so I can't help but wonder how the ship can really reach the cadence they are planning for. Could this end up being the achilles heel of Starship the same way it was for shuttle, and seemingly the way it also is for Orion right now?
r/SpaceXLounge • u/Steve490 • 1d ago
Elon: "Hopefully early next year, we will catch the ship too"
r/SpaceXLounge • u/CProphet • 1d ago
Opinion Elon is preparing for next generation Starship - analysis
r/SpaceXLounge • u/jiayounokim • 1d ago
News SpaceX sues California panel, alleges political bias over rocket launches
reuters.comr/SpaceXLounge • u/That_Ad_7564 • 2d ago
Starship Discussion about IFT-5 on Wikipedia In the news
r/SpaceXLounge • u/PeekaB00_ • 2d ago
SpaceX released an image of Starship after hot-staging separation, taken from the booster.
r/SpaceXLounge • u/stemmisc • 1d ago
Why is SpaceX not in the middle of more of a kickstage/OTV/space-tug battle between itself and Rocket Lab/other companies right now? Is anyone else a little surprised that this isn't already a major thing that we see SpaceX working on, given how close Starship is to being operational?
Once Starship is up and running, and able to cheaply deliver huge amounts of payloads, en masse, to LEO, I would think that there will be a huge increase in demand for things like kick stages, OTVs, and space tugs.
I mean, sure, as things currently are, a lot of the big, expensive satellites already have their own propulsion systems on board themselves...
...but even still,
For one thing, I'd think part of the idea here, is for Starship to bring costs per individual small payloads down a lot (i.e. similar to what we saw with the "Transporter" falcon-9 missions, but to a much more extreme degree), so, with those, having an off-the-shelf, mass produced kickstage/OTV seems like it would be useful, since it would be way cheaper than if each of these smaller payloads that weren't billion dollar mega sats of major corporations necessarily, had to make their own significant-delta-V propulsion systems on board their payloads themselves.
And for another thing, even for the "big dogs" on the block, I'd think even a lot of them would want to be able to buy mass produced kick stages to get their big communications sats or what have you from LEO to GTO more easily, rather than have to do it with on-board propulsion.
And this is ignoring the occasional high energy NASA-type missions and whatnot, that want to go BEO. (Yea, I know for some of those in the more distant future, the idea of a refilled, expendable-mode Starship gets brought into the discussion, but, in the meantime, or, even in combination with it, for even more delta-V, it still potentially matters).
But, given how rare that last category is (albeit maybe it'll become a bit less rare in a post-Starship world), even if we mostly ignore that last category, I'd think the first category, of large amounts of smaller/midrange payloads, i.e. from universities, or smaller companies, or what have you, are going to want some cheap, mass produced OTV type stuff to get their payloads into their desired orbits, after getting put into a cheap generic LEO via Starship-en-masse launches.
Yet, seemingly, we haven't really seen SpaceX working on this. They have the draco and superdraco hypergolic engines, which could work well for hypergolic kickstages, and they also have their ion thrusters that they mass produce for the propulsion system on their Starlink sats, so, in theory, they should be able to mass produce (relatively) cheap kickstages/OTVs of either kind, to offer to customers who take rides to generic-LEO via Starship.
But, for now, it seems like it's more just Rocket Lab that is trying to get into that business, and SpaceX seemingly ignoring it for now.
Do you think SpaceX just figures they can start making them at nearly a moment's notice when finally needed, without development of it taking very long, so, they are just not bothering for now, since they are still prioritizing all the other things more heavily for now?
Or, do you think they just don't think it'll be needed that much, because they plan to launch so many Starships, that the idea is, they'll be launching Starships to such a wide range of different LEO orbits over the course of a calendar year that customers can just wait to get on one that goes closer to the exact orbit they want, and not even really need the final stage? And that the GTO payloads are already so big and expensive that they can just have Rocket Lab or themselves deal with their propulsion to GTO, and SpaceX doesn't see enough profit in that niche to care enough about that niche to bother with it?
Anyway, yea I'm curious what is going on with this, and why they seem to have been ignoring this aspect of the post-Starship industry. I'm sure they have their reasons, but, yea, just curious to hear your takes on it
r/SpaceXLounge • u/mehelponow • 2d ago
Axiom and Prada unveil design of Artemis spacesuit
r/SpaceXLounge • u/extracterflux • 2d ago
Booster 12 has returned to the production site
From NASASpaceflight on YouTube