Space vehicle landing dynamics at failure of landing gear

V. N. Bakulin; S. V. Borzykh; V. V. Voronin

doi:10.3103/S1068799816010049

Space vehicle landing dynamics at failure of landing gear

作者: Bakulin V.N.¹, Borzykh S.V.², Voronin V.V.²
隶属关系:
1. Institute of Applied Mechanics
2. S.P. Korolev Rocket and Space Corporation Energia
期: 卷 59, 编号 1 (2016)
页面: 23-28
栏目: Flight Dynamics and Control of Flight Vehicles
URL: https://journals.rcsi.science/1068-7998/article/view/229540
DOI: https://doi.org/10.3103/S1068799816010049
ID: 229540

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详细

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.