首页> 美国政府科技报告 >Data report for Ames UPWT tests of Apollo 0.105-scale FS-2 static force model at Mach numbers 0.5 to 3.4 to evaluate aerodynamic strakes attached to the command module /fifth series/

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Data report for Ames UPWT tests of Apollo 0.105-scale FS-2 static force model at Mach numbers 0.5 to 3.4 to evaluate aerodynamic strakes attached to the command module /fifth series/

机译：ame UpWT测试阿波罗0.105级Fs-2静力模型的数据报告，马赫数为0.5至3.4，用于评估附在命令模块上的空气动力学条带/第五系列/

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作者
Cummings, D. G.; Hendry, R. G.;
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年度 1963
页码 1-444
总页数 444
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
APOLLO SPACECRAFT; COMMAND MODULES; WIND TUNNEL STABILITY TESTS; SPACECRAFT CONFIGURATIONS; SPACECRAFT DESIGN; SPACECRAFT STABILITY;

机译：apOLLO spaCECRaFT;命令模块;风洞稳定性试验;航天器配置;航天器设计;航天器稳定性;

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3. Appendix C to data report for Ames UPWT tests of Apollo 0.105 scale FS-2 static force model at Mach numbers 0.5 to 3.4 to evaluate aerodynamic strakes attached to the command module /fifth series/ [R] . 1963

机译：ame UpWT测试apollo 0.105规模Fs-2静力模型的数据报告附录C，马赫数为0.5至3.4，用于评估附在命令模块上的空气动力学条带/第五系列/

Data report for Ames UPWT tests of Apollo 0.105-scale FS-2 static force model at Mach numbers 0.5 to 3.4 to evaluate aerodynamic strakes attached to the command module /fifth series/

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