Hot rocket plume experiment: survey and conceptual design

机译：热火箭羽流实验：调查和概念设计

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Abstract: A space-borne engine plume experiment study is underway to fly an experiment which will both verify and quantify the reduced contamination from advanced rhenium-iridium Earth-storable bipropellant rockets (hot rockets) and provide a correlation between high-fidelity, in-space measurements and theoretical plume and surface contamination models. The experiment conceptual design is based upon survey results from plume and contamination technologists throughout the United States.!9

机译：摘要：正在进行一项星载发动机羽流实验研究，以进行一项实验，该实验将验证和量化先进的-铱地球可储存双推进剂火箭（热火箭）所减少的污染，并提供高保真，空间测量以及理论羽流和表面污染模型。实验概念设计基于全美国烟羽和污染技术人员的调查结果！9

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来源
《Optical System Contamination: Effects, Measurement, Control III》|1992年|p.2-13|共12页
会议地点 San Diego CA(US)
作者
Jerry M. Millard; Jet Propulsion Lab.; Downey; CA; USA; Taylor W. Luan; Jet Propulsion Lab.; Pasadena; CA; USA; Mack W. Dowdy; Jet Propulsion Lab.; Pasadena; CA; USA.;
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正文语种 eng
中图分类无线电电子学、电信技术;
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Hot rocket plume experiment: survey and conceptual design

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