首页> 美国政府科技报告 >Pressure and heat transfer tests of the 0.040 scale space shuttle orbiter base heating model (65-0) in the Johnson Space Center space environment simulation laboratory thermal vacuum chamber A, OH79

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Pressure and heat transfer tests of the 0.040 scale space shuttle orbiter base heating model (65-0) in the Johnson Space Center space environment simulation laboratory thermal vacuum chamber A, OH79

机译：约翰逊航天中心空间环境模拟实验室热真空室a，OH79中0.040比例航天飞机轨道器基础加热模型（65-0）的压力和传热测试

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作者
Foust, J. W.;
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年度 1979
页码 1-141
总页数 141
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ENVIRONMENT SIMULATION; FLIGHT TESTS; HEAT TRANSFER; PRESSURE; SPACE SHUTTLE ORBITERS; VACUUM CHAMBERS; WIND TUNNEL TESTS; ASCENT TRAJECTORIES; GIMBALS; HEAT SHIELDING; NOZZLE EFFICIENCY; ROCKET EXHAUST; TECHNOLOGY ASSESSMENT;

机译：环境模拟;飞行测试;传播热量;压力; spaCE sHUTTLE ORBITERs; VaCUUm CHamBERs;风洞隧道测试; asCENT TRaJECTORIEs;万向支架;热屏蔽;喷嘴效率;火箭排气;技术评估;

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Pressure and heat transfer tests of the 0.040 scale space shuttle orbiter base heating model (65-0) in the Johnson Space Center space environment simulation laboratory thermal vacuum chamber A, OH79

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