Testing of Flight Components for the Capillary Pumped Loop Flight Experiment

932235

07/01/1993

Event
International Conference On Environmental Systems
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/932235
Pages
14
Citation
Ottenstein, L., Ku, J., and Butler, D., "Testing of Flight Components for the Capillary Pumped Loop Flight Experiment," SAE Technical Paper 932235, 1993, https://doi.org/10.4271/932235.
Additional Details
Publisher
Published
Jul 1, 1993
Product Code
932235
Content Type
Technical Paper
Language
English