this post was submitted on 04 Oct 2024
28 points (93.8% liked)
Spaceflight
640 readers
73 users here now
Your one-stop shop for spaceflight news and discussion.
All serious posts related to spaceflight are welcome! JAXA, ISRO, CNSA, Roscosmos, ULA, RocketLab, Firefly, Relativity, Blue Origin, etc. (Arca and Pythom, if you must).
Other related space communities:
- !rocketlab@lemmy.nz
- !curiosityrover@lemmy.world
- !perseverancerover@lemmy.world
- !esa@feddit.nl
- !nasa@lemmy.world
- !spacex@sh.itjust.works
- !astronomy@mander.xyz
- !space@lemmy.world
Related meme community:
founded 1 year ago
MODERATORS
you are viewing a single comment's thread
view the rest of the comments
view the rest of the comments
I wonder how much "engine out" capacity they would have on a normal flight. This is a pretty big architectural difference vs Falcon and Starship.
Given that Vulcan has only two BE-4s, I don't expect they would have much capability for engine-out unless it occurred very shortly before scheduled MECO. As for SRB-out capability, that feels like it would depend on the required orbit, SRB configuration, and the exact nature of the failure. They've now demonstrated a certain level of SRB-out capability for the VC2S configuration, but I think a certain amount of luck was involved, in that the rest of the rocket seemingly sustained minimal damage. For the 4- and 6-SRB variants, I think the chances of cascading failures would be higher.