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Providing carrier rocket motion controllability on the basis of design smoothed wind profile application
- Authors: Yendutkina Y.A.1, Titov B.A.2
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Affiliations:
- State Research and Production Space Rocket Center “TsSKB – Progress”, Samara
- Samara State Aerospace University
- Issue: Vol 9, No 4 (2010)
- Pages: 49-57
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/942
- DOI: https://doi.org/10.18287/2541-7533-2010-0-4(24)-49-57
- ID: 942
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Abstract
An algorithm of smoothed wind profile calculating on the basis of the data of atmospheric sounding before the carrier rocket launch has been developed. A method of using design smoothed wind profile in the carrier rocket first stage ascent program for the purpose of providing the controllability under intensive wind perturbations.
About the authors
Ye. A. Yendutkina
State Research and Production Space Rocket Center “TsSKB – Progress”, Samara
Author for correspondence.
Email: endutkina.ea@mail.ru
Head of Group
Russian FederationB. A. Titov
Samara State Aerospace University
Email: Titov@ssau.ru
Doctor of Technical Sciences, Professor
Head of the Department of Logistics and Management in Transport
Russian FederationReferences
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