Email this article Space vehicle landing dynamics at failure of landing gear
- Authors: Bakulin V.N.1, Borzykh S.V.2, Voronin V.V.2
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Affiliations:
- Institute of Applied Mechanics
- S.P. Korolev Rocket and Space Corporation Energia
- Issue: Vol 59, No 1 (2016)
- Pages: 23-28
- Section: 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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Abstract
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.
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About the authors
V. N. Bakulin
Institute of Applied Mechanics
Author for correspondence.
Email: vbak@yandex.ru
Russian Federation, pr. Leningradskii 7, Moscow, 125040
S. V. Borzykh
S.P. Korolev Rocket and Space Corporation Energia
Email: vbak@yandex.ru
Russian Federation, ul. Lenina 4a, Korolev, Moscow oblast, 141070
V. V. Voronin
S.P. Korolev Rocket and Space Corporation Energia
Email: vbak@yandex.ru
Russian Federation, ul. Lenina 4a, Korolev, Moscow oblast, 141070
