Analysis of the spacecraft vertical landing dynamics on the platform with crash legs
- Авторлар: Shcheglov G.A.1, Lukovkin R.O.1
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Мекемелер:
- Bauman Moscow State Technical University
- Шығарылым: Том 60, № 3 (2017)
- Беттер: 382-390
- Бөлім: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230189
- DOI: https://doi.org/10.3103/S1068799817030090
- ID: 230189
Дәйексөз келтіру
Аннотация
This paper proposes a novel landing gear for spacecraft that allows a weight reduction due to using deformable crash legs. Numerical simulation of the landing process was performed.
Негізгі сөздер
Авторлар туралы
G. Shcheglov
Bauman Moscow State Technical University
Хат алмасуға жауапты Автор.
Email: shcheglov_ga@bmstu.ru
Ресей, ul. Vtoraya Baumanskaya 5, Moscow, 105005
R. Lukovkin
Bauman Moscow State Technical University
Email: shcheglov_ga@bmstu.ru
Ресей, ul. Vtoraya Baumanskaya 5, Moscow, 105005
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