Displacement simulation for spacecraft structure
- 作者: Senashov S.N.1, Balyakov D.F.2
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隶属关系:
- Reshetnev Siberian State Aerospace University
- Reshetnev AO ISS
- 期: 卷 60, 编号 1 (2017)
- 页面: 57-63
- 栏目: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/229991
- DOI: https://doi.org/10.3103/S1068799817010093
- ID: 229991
如何引用文章
详细
The paper presents a technique of forming and evaluating the allowable clearance between a launch vehicle fairing and spacecraft.
作者简介
S. Senashov
Reshetnev Siberian State Aerospace University
Email: d-bolyakov@iss-reshetnev.ru
俄罗斯联邦, pr. imeni gazety “Krasnoyarskii rabochii” 31, Krasnoyarsk
D. Balyakov
Reshetnev AO ISS
编辑信件的主要联系方式.
Email: d-bolyakov@iss-reshetnev.ru
俄罗斯联邦, ul. Lenina 52, Zheleznogorsk, Krasnoyarskii krai, 662972
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