Aerodynamic Control System for a Deployable Re-entry Capsule

Acta Astronautica(2021)

Cited 27|Views4
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Abstract
Deployable aerobrakes for Earth re-entry capsules may offer many advantages in the near future, including the opportunity to recover on Earth payloads and samples from Space with reduced risks and costs with respect to conventional systems. Such capsules can be accommodated in the selected launcher in folded configuration, optimizing the available volume, and when foreseen by the mission profile the aerobrake can be deployed in order to increase the surface exposed to the hypersonic flow and therefore to reduce the ballistic parameter.
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Key words
Re-entry vehicle,Deployable heat shield,Flaps,LQR controller
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