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Starship Flight 5: Launch and booster catch [video]

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Re: Starship Flight 5: Launch and booster catch [video]

#221
post #200

What does Starship reusability mean for $/kg to LEO? I know there are longer term targets of $10/kg but that supposes efficiencies that aren’t here yet. Would be helpful to understand before Starship reusability where the state of the art was in terms of $/kg to LEO and where we would be with impending Starship reusability.

https://www.reddit.com/r/SpaceXLounge/comments/1bgmsm9/cost_...

Re: Starship Flight 5: Launch and booster catch [video]

#222

It's difficult to overstate how important the milestone of catching the booster is. Now we have a reusable rocket an order of magnitude larger than anything we've had before, and the cost of kg to orbit just nosedived.

They're a long way from having a reusable super heavy booster. It's still copping a lot of damage on the landing.

true but don't forget this is test flight #5

Re: Starship Flight 5: Launch and booster catch [video]

#224
post #183

Earlier quoted context omitted.

MIMO and nonlinear control theories are probably some of the hardest topics in all of engineering. SpaceX control system also has to compensate for the fuel moving inside their rockets so the control algorithms probably involve some kind of fast numerical fluid simulation. Another interesting thing SpaceX is doing is to use consumer-grade chips in triple redundancy configurations instead of using $100,000+ radiation-…

I always thought the liquid sloshing would be one of the hardest to simulate (considering how chaotic fluid mechanics is). Interestingly, I think this caused the 2nd Falcon launch to fail (the LOX sloshing).

I think some Kerbel Space Program players have attempted to approximate the liquid sloshing as an inverted single or double pendulum problem inside the rocket that the control algorithm has to take into consideration in addition to the primary control of the rocket.

Re: Starship Flight 5: Launch and booster catch [video]

#225

Closeup of chopsticks as they were catching the booster, best clip from Everyday Astronaut's livestream: https://x.com/kagurazakimoto/status/1845447451592765820

I'd never considered a 70m tall chunk of mostly metal "agile", but the way it's controlled into the arms so precisely is something to behold.

Re: Starship Flight 5: Launch and booster catch [video]

#226
post #200

What does Starship reusability mean for $/kg to LEO? I know there are longer term targets of $10/kg but that supposes efficiencies that aren’t here yet. Would be helpful to understand before Starship reusability where the state of the art was in terms of $/kg to LEO and where we would be with impending Starship reusability.

I don't think we have a number for it yet. But it will definitely be the cheapest launch system at the time of launch.

People say 200$/kg just with booster reuse, and 20$/kg with full reuse. Of course this might be too optimistic, but I truly believe we might reach under 50$ in this decade.

Re: Starship Flight 5: Launch and booster catch [video]

#228
post #23

Nothing could have prepared me for how that catch looked. I was sure the rocket was careening into the tower at the last second before it straightened out. The control algorithms must be incredible for the landing system to work within those small tolerances.

timestamp for "catch" is around 40:00 for those curious

Re: Starship Flight 5: Launch and booster catch [video]

#229
post #23

Nothing could have prepared me for how that catch looked. I was sure the rocket was careening into the tower at the last second before it straightened out. The control algorithms must be incredible for the landing system to work within those small tolerances.

When Musk first proposed this, I thought he was crazy. It seemed like something a school boy would draw up. Now I think this will become routine and forgettable after a few more successes. Is there a word for that - something out of fiction becoming mundane?

Re: Starship Flight 5: Launch and booster catch [video]

#230
post #23

Nothing could have prepared me for how that catch looked. I was sure the rocket was careening into the tower at the last second before it straightened out. The control algorithms must be incredible for the landing system to work within those small tolerances.

The booster was falling at 4500 Km/h 30 seconds before the catch with 2-3% fuel left. How is that amount of fuel remotely enough to stop the downward momentum?
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