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This study proposes a novel rebound suppression mechanism for celestial landing problem, consisting of additional mass and spring, can be achieved by the lightweight and low-complexity system. It considers into account the characteristics of both mechanical energy and momentum exchange simultaneously.

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This page is a summary of: Conceptual Study on Robust Rebound Suppression Mechanism for Small-Body Landing, Journal of Spacecraft and Rockets, November 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34817.
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