Estimation of atmospheric parameters for determining dispersion ellipses of space rocket fragments

被引：0
|
作者：
Borisov, A. A. [1 ]
Gotyur, I. A. [1 ]
Kuleshov, Yu. V. [1 ]
Makov, A. B. [1 ]
Suvorov, S. S. [1 ]
Shchukin, G. G. [1 ]
机构：
[1] Mozhaiskii Mil Space Acad, Ul Zhdanovskaya 13, St Petersburg 197082, Russia
来源：
RUSSIAN METEOROLOGY AND HYDROLOGY | 2017年 / 42卷 / 05期
关键词：
Ballistic calculations; dispersion ellipse; impact area of space rocket modules; mathematical model of the atmosphere; accident launch; estimation of atmospheric parameters; coordinate functions of atmospheric parameters;
D O I：
10.3103/S1068373917050041
中图分类号：
P4 [大气科学（气象学）];
学科分类号：
0706 ; 070601 ;
摘要：
A new approach to the estimation of atmospheric parameters affecting the movement of space rocket fragments in case of accident launches is proposed by the example of the Plesetsk Cosmodrome. Due to the absence of operational information on the vertical distribution of atmospheric parameters above 30 km, the method is considered which allows using available archival aerological data and the statistical characteristics of air density and wind speed components computed from the rocket sounding of the atmosphere for ballistic calculations.
引用
收藏
页码：299 / 304
页数：6
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