Can Space X Integrate Autorotation in Reusable Rockets?

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SpaceX is exploring the development of a reusable rocket but has not adopted the idea of integrating autorotation with a foldable rotor for landing. While autorotation could save fuel, it introduces challenges such as increased dead weight from the rotor and limited maneuverability. The current design of SpaceX's reusable booster is lightweight, allowing for efficient fuel use during landing. The primary obstacle remains achieving effective engine throttling. Overall, while the autorotation concept has potential, it may not align with SpaceX's current design goals.
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Space X wants to build such a reusable rocket:
Why don't they instead use a foldable rotor and land the thing with autorotation?
I mean it wouldn't take any fuel.
 
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There was one contender that had such a design, but they dropped out early in the competition.
Do note that the rotor idea has some disadvantages, as it adds the dead weight of large hinged blades and their attachments, plus unpowered it has very limited maneuverability.
The Space X reusable booster requires very little fuel, as the empty booster is a fraction of the weight of the full unit. Throttling the engine efficiently is the biggest challenge, but if that is achieved, landing for reuse is a realistic option.
 
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Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming up shortly, I'll be following up afterwards to see how it all goes. :smile: https://blogs.nasa.gov/spacex/
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