Physical and Mathematical Simulation of Electric Polarization of Low-Orbit Spacecraft under the Conditions of Hypersonic Flow by a Stream of Plasma of the Earth's Upper Ionosphere

被引：0
作者：
I. Yu. Skryabysheva
机构：
[1] Central Research Institute of Mechanical Engineering,
来源：
Cosmic Research | 2004年 / 42卷
关键词：
Calculation Result; Theoretical Concept; Mathematical Simulation; Electric Polarization; Hypersonic Flow;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The charging processes in the vicinity of a low-orbital spacecraft moving in the midlatitude ionosphere are considered. It is shown that the main feature of charging of such an object is its polarization. The calculation results are analyzed in the context of general theoretical concepts.
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页码：39 / 47
页数：8
相关论文
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