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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Bibliographische Detailangaben
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
Online-Zugang:	Volltext
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Beschreibung
Zusammenfassung:	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.
ISSN:	1068-7998 1934-7901
DOI:	10.3103/S1068799817030090