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Questions about a craft used to propel payloads into space, usually a rocket-powered vehicle

2 votes
1 answer
140 views

Accidents where discarded stages are propelled by vaporized propellant?

Falcon 1 flight 3 failed when propellant vaporized in the detached first stage's engine, causing it to slam into the second stage. Has this happened to any other launch vehicle? Do launch vehicles usu …
Abdullah is not an Amalekite's user avatar
8 votes
2 answers
487 views

How will Starship get ullage during launch?

All the Starship air-starts up to this point have been landing burns using small header tanks which gave less ullage requirements, but I can't recall any mention of how Starship settle it's propellant …
Abdullah is not an Amalekite's user avatar
1 vote
0 answers
78 views

What if satellites could be recovered during a launch failure? [duplicate]

How heavy would a capsule have to be to return a satellite safely to earth in the event of a launch failure? Would a satellite survive the loads endured by astronauts during an abort? If not, is there …
Abdullah is not an Amalekite's user avatar
1 vote
1 answer
525 views

Why was the launchpad not destroyed during Super Heavy test firings?

It's becoming clear now that the 4/20 launch devastated the launchpad, leaving a massive crater and flinging debris - perhaps into the booster itself. But why did this not happen during test firings o …
Abdullah is not an Amalekite's user avatar
1 vote
2 answers
350 views

Why didn't SpaceX scrub the 4/20 Starship launch when they saw the launch pad being shredded?

While Starship took to the skies on its maiden flight, the slow build of power started to devastate the launch pad (or Stage Zero as SpaceX refers to it) and surrounding area with debris. Though curr …
Abdullah is not an Amalekite's user avatar
11 votes
1 answer
4k views

Does a fully loaded Starship really have a thrust to weight ratio less than 1 at sea level?

If Superheavy fails during launch (or even fails to launch in an unsafe way) the Starship itself might well be able to just light its engines and fly a suitable suborbital trajectory https://space.s …
Abdullah is not an Amalekite's user avatar
5 votes
0 answers
196 views

Low-pressure pump-fed rocket engine?

I saw the above suggested in LEO on the Cheap. In P.130 it says: A compromise between high-performance/lightweight pump-fed vehicle designs and cost-optimized pressure-fed vehicles with heavier struc …
Abdullah is not an Amalekite's user avatar
1 vote
0 answers
52 views

Launch excapse system for satellite payloads? [duplicate]

Once a rocket lifts off, there is usually no abort mode that does not involve the destruction of the rocket, and on a satellite launch, the payload. Therefore, expendeble satellite launchers are quite …
Abdullah is not an Amalekite's user avatar
5 votes
1 answer
435 views

Why wasn't Buran mounted on top of Energia?

Since unlike the Shuttle, the Buran did not carry the main engines, why was it not mounted on top of the external tank equivalent - Energia's core stage? And even better, why wasn't Energia's second s …
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