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Testing of Flight Components for the Capillary Pumped Loop Flight Experiment NASA/Goddard Space Flight Center

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Ottenstein, Laura, author.
Conference Name:
International Conference On Environmental Systems (1993-07-12 : Colorado Springs, Colorado, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1993
Summary:
The Capillary Pumped Loop Flight Experiment (CAPL) is a prototype of the Earth Observing System (EOS) instrument thermal control systems. Four CAPL flight hardware components were tested in the Instrument Thermal Test Bed at NASA's Goddard Space Flight Center. The components tested were the capillary cold plates, capillary starter pump, heat pipe heat exchangers (HPHXs), and reservoir. The testing verified that all components meet or exceed their individual performance specifications. Consequently, the components have been integrated into the CAPL experiment which will be flown on the Space Shuttle in late 1993
Notes:
Vendor supplied data
Publisher Number:
932235
Access Restriction:
Restricted for use by site license

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