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I wonder if the Falcon Heavy is going to attempt a second stage recovery. While the first stage recovery is impressive and still a serious money saver, it's also not quite as necessary to use the thrusters.
It'd be crazy to see a second stage booster make it back like the original plan though. At that altitude, the rocket thrust might be the only option to keep it from burning up since the boosters probably can't be too heavily shielded. I guess falcon 9 never tried it since the payload cost was too high.
There was talk of attempting second stage recovery, it's far more challenging than first stage recovery though. It's going a whole hell of a lot faster than the first stage. The nozzle on the Merlin Vacuum engine is far larger and more fragile too, plus the second stage lacks cold gas thrusters and grid fins for attitude control. Definitely very challenging.
Yep. I know they've tested relighting on the second stage with F9, but it'd definitely be something else if they can recover it of heavy. Still don't know if that's going to be attempted on the upcoming launch or not.
It'd definitely be a more revolutionary step since first stage recoveries in general weren't exactly new when F9 had its first vertical landing, and the SpaceX goal has been full recovery of the booster rocket.
Either way, definitely looking forward to the launch.
Wish I was in FL still to watch it.
Second stage re-light is proven. They use it on plenty of launches, not sure how many they have per launch, but it's used already.
As for the recovery part, the idea maybe isn't new, but no one had actually done it with an orbital class rocket before SpaceX. The closest was probably the DC-X: https://en.wikipedia.org/wiki/McDonnell_Douglas_DC-X
The Space Shuttle doesn't really count, as much as I love it.
Yeah. Pretty sure relight has been tested on almost every recent generation F9 from the launches I've watched. I do wonder how much higher the F9 first stage separation happens than the SS boosters now that I think about it. Both happen in the upper stratosphere iirc.
I just want to see a second stage come back. No orbital booster has ever been recovered completely. SS is probably the closest thing, but the tank had to be jetisoned.
Talking about the reusability of the space shuttle during the Reagan administration, it cost ~$1 billion to get a shuttle ready to launch again. This was not reported at the time as NASA wanted the populace to believe these shuttles were as reusable as a 747. Nothing could be further from the truth.
The space shuttle lands like a brick and is much rebuilt each time, not really a reusable space plane, more of a plane shaped rocket with solid fuel boosters.
I loved the concept but we could have done a lot more with the money using conventional rockets as the space shuttle only carried 1.3% of it's total weight as payload.
Why not build a space plane that could be piggybacked into the thin air then power itself from there? Getting off the ground and to the edge of gravity is the expensive part, a 2 part space plane would make sense, even if they were smaller.
Here's a cool look at Falcon heavy : Falcon Heavy | SpaceX
The space shuttle lands like a brick and is much rebuilt each time, not really a reusable space plane, more of a plane shaped rocket with solid fuel boosters.
I loved the concept but we could have done a lot more with the money using conventional rockets as the space shuttle only carried 1.3% of it's total weight as payload.
Why not build a space plane that could be piggybacked into the thin air then power itself from there? Getting off the ground and to the edge of gravity is the expensive part, a 2 part space plane would make sense, even if they were smaller.
Here's a cool look at Falcon heavy : Falcon Heavy | SpaceX