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Analytical model for determining spacecraft impact velocity and orientation relative to an impact surface

机译：用于确定航天器撞击速度和相对于撞击表面的方向的分析模型

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摘要

Development of analytical model for determining spacecraft impact velocity and orientation relative to impact surface for variable dynamic conditions

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作者
Howes, D. B.; Whitnah, A. M.;
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年度 1971
页码 1-20
总页数 20
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
DECELERATION; IMPACT ACCELERATION; IMPACT LOADS; SPACECRAFT LANDING; NUMERICAL ANALYSIS; PERFORMANCE PREDICTION; SPACECRAFT PERFORMANCE;

机译：DECELERaTION;影响加速;影响负荷;航天飞机着陆;数值分析;绩效预测;航天器性能;

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8. Analytical Model for Determining Spacecraft Impact Velocity and Orientation Relative to an Impact Surface [R] . Howes, D. B., Whitnah, A. M. 1971

机译：确定航天器相对于冲击面的冲击速度和方向的分析模型

Analytical model for determining spacecraft impact velocity and orientation relative to an impact surface

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