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Heat Pipe Technology for Current Spacecraft and High Power Thermal Management OAO Corporation Greenbelt, Maryland

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Kroliczek, E., author.
Conference Name:
Intersociety Conference on Environmental Systems (1985-07-15 : San Francisco, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1985
Summary:
The application of conventional axially grooved heat pipes to the thermal control of attached shuttle payloads, instruments on free flyers, communications satellites and body mounted radiators for space station common modules is discussed. Also presented is the evolution of an advanced axially grooved design for application to the space station's space erectible radiators (SERS). Capillary Pumped Loop (CPL) development status and its application to high power thermal management for space station applications are also included
Notes:
Vendor supplied data
Publisher Number:
851353
Access Restriction:
Restricted for use by site license

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