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Telemetry measurements of afterbody pressures on free-flying models of the Apollo capsule at Mach numbers from 10 to 21 in helium and 14 in air

机译：apollo舱的自由飞行模型的后体压力的遥测测量，氦气中的马赫数为10至21，空气中为14

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Kemp, J. H., Jr.;
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年度 1965
页码 1-36
总页数 36
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; APOLLO SPACECRAFT; COMMAND MODULES; PRESSURE DISTRIBUTION; WIND TUNNEL MODELS; AERODYNAMIC CONFIGURATIONS; FREE FLIGHT; HYPERVELOCITY WIND TUNNELS; TELEMETRY;

机译：空气动力学特征; apOLLO spaCECRaFT;命令模块;压力分布;风洞模型;空气动力学配置;免费飞行; HYpERVELOCITY WIND TUNNELs;遥测;

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专利

1. FM Telemetry for Multiple Force Measurements on Free-Flying Models [J] . Harrison Dean R., Coon Grant W., Mateer George G., Aerospace and Electronic Systems, IEEE Transactions on . 1968,第2期

机译：FM遥测，用于自由飞行模型上的多力测量
2. Mach 10 Rayleigh Scattering Gas-Cap Density, Pressure, and Shock-Jump Measurements [J] . Balla R. Jeffrey AIAA Journal . 2015,第3期

机译：马赫数10瑞利散射气帽密度，压力和冲击跳跃测量
3. Supersaturation Total Temperature, Pitot Pressure, and Rayleigh Scattering Measurements at Mach 10 [J] . R. Jeffrey Balla, Matthew N. Rhode, Joel L. Everhart AIAA Journal . 2014,第7期

机译：10马赫时过饱和总温度，皮托管压力和瑞利散射测量
4. Heat Flux Measurement of Apollo Capsule Model at High Stagnation Pressure in Shock Tunnel HIEST [C] . Tanno Hideyuki, Komuro Tomoyuki, Sato Kazuo, 22nd AIAA international space planes and hypersonic systems and technologies conference . 2018

机译：冲击隧道HIEST中高停滞压力下阿波罗胶囊模型的热通量测量
5. Experimental pressure and heat transfer investigation over a "directed-energy air spike" inlet at flow mach numbers of 10 to 20, stagnation temperature of 1000 K, and arc powers up to 127 KW. [D] . Toro, Paulo Gilberto de Paula. 1998

机译：在流量为10至20的马赫数，停滞温度为1000 K，电弧功率高达127 KW的“定向能空气尖峰”入口上进行实验压力和传热研究。
6. In vivo measurement of intrauterine pressure by telemetry: a new approach for studying parturition in mouse models [O] . Stephanie L. Pierce, William Kutschke, Rafael Cabeza, -1

机译：遥测在体内测量子宫内压：研究小鼠模型中分娩的新方法
7. Experimental results of a Mach 10 conical-flow derived waverider to 14-X hypersonic airspace vehicle [O] . Tiago Cavalcanti Rolim, Paulo Gilberto de Paula Toro, Marco Antonio Sala Minucci, 2011

机译：Mach 10锥形流动推导波浪员的实验结果到14-x超声波空间车辆

Telemetry measurements of afterbody pressures on free-flying models of the Apollo capsule at Mach numbers from 10 to 21 in helium and 14 in air

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