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, Issue 8(74),Pages <nobr>118

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

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.

UDC: 629.78

Received: 21.09.2009
Revised: 21.09.2009