Space vehicle landing dynamics at failure of landing gear
- Авторлар: Bakulin V.1, Borzykh S.2, Voronin V.2
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Мекемелер:
- Institute of Applied Mechanics
- S.P. Korolev Rocket and Space Corporation Energia
- Шығарылым: Том 59, № 1 (2016)
- Беттер: 23-28
- Бөлім: 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
Дәйексөз келтіру
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.
Негізгі сөздер
Авторлар туралы
V. Bakulin
Institute of Applied Mechanics
Хат алмасуға жауапты Автор.
Email: vbak@yandex.ru
Ресей, pr. Leningradskii 7, Moscow, 125040
S. Borzykh
S.P. Korolev Rocket and Space Corporation Energia
Email: vbak@yandex.ru
Ресей, ul. Lenina 4a, Korolev, Moscow oblast, 141070
V. Voronin
S.P. Korolev Rocket and Space Corporation Energia
Email: vbak@yandex.ru
Ресей, ul. Lenina 4a, Korolev, Moscow oblast, 141070