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Ground Tests of Capillary Pumped Loop (CAPL 3) Flight Experiment NASA Goddard Space Flight Center

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Ku, Jentung, author.
Conference Name:
International Conference On Environmental Systems (1998-07-13 : Danvers, Massachusetts, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1998
Summary:
The success of CAPL 2 flight experiment has stirred many interests in using capillary pumped loop (CPL) devices for spacecraft thermal control. With only one evaporator in the loop, CAPL 2 was considered a point design for the Earth Observing System (EOS-AM). To realize the full benefits of CPLs, a reliable system with multiple evaporators must be developed and successfully demonstrated in space. The Capillary Pumped Loop (CAPL 3) Flight Experiment was designed to flight demonstrate a multiple evaporator CPL in a space environment. New hardware and concepts were developed for CAPL 3 to enable reliable start-up, constant conductance operation, and heat load sharing. A rigorous ground test program was developed and extensive characterization tests were conducted. All performance requirements were met, and the loop demonstrated very reliable operation
Notes:
Vendor supplied data
Publisher Number:
981812
Access Restriction:
Restricted for use by site license

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