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