Отправить статью по E-mail Space vehicle landing dynamics at failure of landing gear
- Авторы: Bakulin V.1, Borzykh S.2, Voronin V.2
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Учреждения:
- Institute of Applied Mechanics
- S.P. Korolev Rocket and Space Corporation Energia
- Выпуск: Том 59, № 1 (2016)
- Страницы: 23-28
- Раздел: 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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Аннотация
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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Об авторах
V. Bakulin
Institute of Applied Mechanics
Автор, ответственный за переписку.
Email: vbak@yandex.ru
Россия, pr. Leningradskii 7, Moscow, 125040
S. Borzykh
S.P. Korolev Rocket and Space Corporation Energia
Email: vbak@yandex.ru
Россия, ul. Lenina 4a, Korolev, Moscow oblast, 141070
V. Voronin
S.P. Korolev Rocket and Space Corporation Energia
Email: vbak@yandex.ru
Россия, ul. Lenina 4a, Korolev, Moscow oblast, 141070
