Design requirements for spacecraft heat rejection systems are indentified, and their impact on the construction of conventional pumped fluid and hybrid heat pipe/pumped fluid radiators is evaluated. Heat rejection systems to improve the performance or reduce the cost of the spacecraft are proposed. Heat rejection requirements which are large compared to those of existing systems and mission durations which are relatively long, are discussed.
Spacecraft Radiators for Advanced Mission Requirements
1980
134 pages
Report
Keine Angabe
Englisch
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