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Vestnik SamGU. Estestvenno-Nauchnaya Ser., 2009, Issue 8(74), Pages 118–124 (Mi vsgu286)  
Mechanics

Principles of forming of the wind profiles, used for the flight programme aimed at reduction of loading on the carrier rocket

V. V. Dmitriev, E. A. Endutkina

State Research and Production Space-Rocket Center "TsSKB-Progress", Samara, 443009, Russia
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Abstract: One of the primal functions of a carrier rocket control system consists in assurance of motion stability under wind impact conditions. Here a technique for forming of wind profiles used for the calculation of ascent programs done according to pre-launch measurements of wind speed is proposed.
Keywords: carrier rocket, control system, motion stability, angle of incidence (slide), atmospheric sounding, wind profile, carrier rocket ascent program.
Received: 21.09.2009
Revised: 21.09.2009
Document Type: Article
UDC: 629.78
Language: Russian
Citation: V. V. Dmitriev, E. A. Endutkina, “Principles of forming of the wind profiles, used for the flight programme aimed at reduction of loading on the carrier rocket”, Vestnik Samarskogo Gosudarstvennogo Universiteta. Estestvenno-Nauchnaya Seriya, 2009, no. 8(74), 118–124
Citation in format AMSBIB
\Bibitem{DmiEnd09}
\by V.~V.~Dmitriev, E.~A.~Endutkina
\paper Principles of forming of the wind profiles, used for the flight programme aimed at reduction of loading on the carrier rocket
\jour Vestnik Samarskogo Gosudarstvennogo Universiteta. Estestvenno-Nauchnaya Seriya
\yr 2009
\issue 8(74)
\pages 118--124
\mathnet{http://mi.mathnet.ru/vsgu286}
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    		Вестник Самарского государственного университета. Естественнонаучная серия
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    References:33
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