ISSN 0021-3454 (print version)
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vol 64 / March, 2021
Article

DOI 10.17586/0021-3454-2016-59-4-268-274

UDC 629.191

METHOD OF ATMOSPHERIC MODEL REFINEMENT FOR BALLISTIC SUPPORT OF ROCKET-CARRIER LAUNCHES

V. N. Arseniev
A. F. Mozhaysky Military Spaсe Academy, Department of Onboard Information and Measuring Complexes; Professor


A. B. Kuznetsov
Mozhaysky Military Space Academy, Department of Automated Systems of Preparation and Launch of Space Appointment Rockets, St. Petersburg;


A. A. Yadrenkin
A. F. Mozhaisky Military Space Academy, Department of On-board Information and Measuring Complexes; Associate Professor


Abstract. The problem of refinement of atmospheric model used for ballistic support of rocket-carrier launch is considered. The vertical profiles of thermodynamic parameters of the atmosphere and wind velocity are presented in the form of canonical decompositions with known mean values, mean square deviations, and coordinate functions in node points along the vertical coordinate. The proposed approach allows approximating the specified characteristics of atmospheric parameters dispersion with the model ones.
Keywords: rocket-carrier, separating part, movement forecasting, model of the atmosphere, ballistic support

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