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

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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Veröffentlicht in:	Russian aeronautics 2017-07, Vol.60 (3), p.382-390
Hauptverfasser:	Shcheglov, G. A., Lukovkin, R. O.
Format:	Artikel
Sprache:	eng
Schlagworte:	Automotive Engineering Engineering Flight Dynamics and Control of Flight Vehicles
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description	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.
doi_str_mv	10.3103/S1068799817030090
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source	Springer Nature - Complete Springer Journals
subjects	Automotive Engineering Engineering Flight Dynamics and Control of Flight Vehicles
title	Analysis of the spacecraft vertical landing dynamics on the platform with crash legs
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