Testing of Flight Components for the Capillary Pumped Loop Flight Experiment

Document Number: 932235

Date Published: July 1993

Author(s):
Laura Ottenstein - NASA Goddard Space Flight Center
Jentung Ku - NASA Goddard Space Flight Center
Dan Butler - NASA Goddard Space Flight Center

Abstract:
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

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Product Status: In Stock

See other papers presented at International Conference On Environmental Systems, July 1993, Colorado Springs, CO, USA, Session: International Conference On Environmental Systems

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