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J.K. Lund's avatar

First stage rocket reuse was solved by SpaceX: Simply keep extra fuel in reserve, fall to the ground, and use your existing engines to land.

Second stage reuse is a much bigger challenge because the energies involved are far too high to do the same. There are three main approaches to this problem:

1) Space Shuttle type winged landing

2) SpaceX's belly flop

3) Stokes dual use aerospike engine.

The problem with winged landings is that wings add a lot of weight and are useless outside the atmosphere. It also requires tens of thousands of protective tiles.

SpaceX's Starship gets around this by using movable fins to control the initial reentry, then using its engines to flip it upright for landing. Though it still needs protective tiles.

Stoke's approach is my favorite. Instead of fins, wings, and tiles, Stoke uses a hydrogen-fueled, quasi aerospike, expander cycle engine the second stage for ascent.

Then, on decent, they reenter with that 'aerospike' windward and run the expander cycle with the engine nozzles closed. Using the rockets own fuel to cool it down.

This makes brilliant use of the hardware and saves mass. The engines, already capable of withstanding extreme heat on ascent, are also used for decent. No separate hardware required:

https://www.lianeon.org/p/the-race-for-the-holy-grail-of-rocketry

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