Space vehicle landing dynamics at failure of landing gear

In this paper, we consider the dynamics of the space vehicle motion at interaction with soil surface in the case of landing gear failure. The time dependences are obtained for the landing parameters such as overloads, linear velocity of the center of mass, angular velocity of the vehicle, and cleara...

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Veröffentlicht in:	Russian aeronautics 2016, Vol.59 (1), p.23-28
Hauptverfasser:	Bakulin, V. N., Borzykh, S. V., Voronin, V. V.
Format:	Artikel
Sprache:	eng
Schlagworte:	Automotive Engineering Engineering Flight Dynamics and Control of Flight Vehicles
Online-Zugang:	Volltext
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Beschreibung
Zusammenfassung:	In this paper, we consider the dynamics of the space vehicle motion at interaction with soil surface in the case of landing gear failure. The time dependences are obtained for the landing parameters such as overloads, linear velocity of the center of mass, angular velocity of the vehicle, and clearance. The criticality degree in the case of failure is evaluated.
ISSN:	1068-7998 1934-7901
DOI:	10.3103/S1068799816010049