An investigation was made to formulate and evaluate heat pipe applications for the space shuttle orbiter. Of the twenty-seven specific applications which were identified, a joint evaluation resulted in the selection of five of the most promising ones for prototype development. The formulation process is described, along ns which evolved. The bulk of the discussion deals with the top five applications: (1) heat pipe augmented cold rail; (2) avionics heat pipe circuit; (3) heat pipe/phase change material modular sink; (4) air-to-heat-pipe heat exchanger; and (5) heat pipe radiator for compartment temperature control. The philosophy, physical design details, and performance data are presented for each concept along with a comparison to the baseline design where applicable. A sixth application, heat pipe space radiator for waste heat rejection, was also recommended for prototype development. (Author)
Space Shuttle Orbiter Heat Pipe Applications. Volume 1 Synopsis
1972
88 pages
Report
No indication
English
Space Shuttle Orbiter Barricade
NTIS | 1974
|Space shuttle orbiter avionics
Tema Archive | 1977
|NTIS | 1994