Email this article Displacement simulation for spacecraft structure
- Authors: Senashov S.N.1, Balyakov D.F.2
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Affiliations:
- Reshetnev Siberian State Aerospace University
- Reshetnev AO ISS
- Issue: Vol 60, No 1 (2017)
- Pages: 57-63
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/229991
- DOI: https://doi.org/10.3103/S1068799817010093
- ID: 229991
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Abstract
The paper presents a technique of forming and evaluating the allowable clearance between a launch vehicle fairing and spacecraft.
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About the authors
S. N. Senashov
Reshetnev Siberian State Aerospace University
Email: d-bolyakov@iss-reshetnev.ru
Russian Federation, pr. imeni gazety “Krasnoyarskii rabochii” 31, Krasnoyarsk
D. F. Balyakov
Reshetnev AO ISS
Author for correspondence.
Email: d-bolyakov@iss-reshetnev.ru
Russian Federation, ul. Lenina 52, Zheleznogorsk, Krasnoyarskii krai, 662972
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