Email this article Analysis of the spacecraft vertical landing dynamics on the platform with crash legs
- Authors: Shcheglov G.A.1, Lukovkin R.O.1
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Affiliations:
- Bauman Moscow State Technical University
- Issue: Vol 60, No 3 (2017)
- Pages: 382-390
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/230189
- DOI: https://doi.org/10.3103/S1068799817030090
- ID: 230189
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Abstract
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.
About the authors
G. A. Shcheglov
Bauman Moscow State Technical University
Author for correspondence.
Email: shcheglov_ga@bmstu.ru
Russian Federation, ul. Vtoraya Baumanskaya 5, Moscow, 105005
R. O. Lukovkin
Bauman Moscow State Technical University
Email: shcheglov_ga@bmstu.ru
Russian Federation, ul. Vtoraya Baumanskaya 5, Moscow, 105005
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