Analysis of the spacecraft vertical landing dynamics on the platform with crash legs


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This paper proposes a novel landing gear for spacecraft that allows a weight reduction due to using deformable crash legs. Numerical simulation of the landing process was performed.

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G. Shcheglov

Bauman Moscow State Technical University

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Email: shcheglov_ga@bmstu.ru
俄罗斯联邦, ul. Vtoraya Baumanskaya 5, Moscow, 105005

R. Lukovkin

Bauman Moscow State Technical University

Email: shcheglov_ga@bmstu.ru
俄罗斯联邦, ul. Vtoraya Baumanskaya 5, Moscow, 105005

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