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Proceedings Paper

Hot rocket plume experiment: survey and conceptual design
Author(s): Jerry M. Millard; Taylor W. Luan; Mack W. Dowdy
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Paper Abstract

Attention is given to a space-borne engine plume experiment study 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 on survey results from plume and contamination technologists throughout the U.S. With respect to shuttle use, cursory investigations validate Hitchhiker availability and adaptability, adequate remote manipulator system (RMS) articulation and dynamic capability, acceptable RMS attachment capability, adequate power and telemetry capability, and adequate flight altitude and attitude/orbital capability.

Paper Details

Date Published: 18 December 1992
PDF: 12 pages
Proc. SPIE 1754, Optical System Contamination: Effects, Measurement, Control III, (18 December 1992); doi: 10.1117/12.140720
Show Author Affiliations
Jerry M. Millard, Jet Propulsion Lab. (United States)
Taylor W. Luan, Jet Propulsion Lab. (United States)
Mack W. Dowdy, Jet Propulsion Lab. (United States)


Published in SPIE Proceedings Vol. 1754:
Optical System Contamination: Effects, Measurement, Control III
A. Peter M. Glassford, Editor(s)

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