Enviar artigo por via de e-mail Analysis of the spacecraft vertical landing dynamics on the platform with crash legs
- Autores: Shcheglov G.A.1, Lukovkin R.O.1
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Afiliações:
- Bauman Moscow State Technical University
- Edição: Volume 60, Nº 3 (2017)
- Páginas: 382-390
- Seção: 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
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Resumo
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.
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Sobre autores
G. Shcheglov
Bauman Moscow State Technical University
Autor responsável pela correspondência
Email: shcheglov_ga@bmstu.ru
Rússia, ul. Vtoraya Baumanskaya 5, Moscow, 105005
R. Lukovkin
Bauman Moscow State Technical University
Email: shcheglov_ga@bmstu.ru
Rússia, ul. Vtoraya Baumanskaya 5, Moscow, 105005
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