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HEPP - A low temperature Heat Pipe Experiment Package developed for flight on-board the Long Duration Exposure Facility /LDEF/The Heat Pipe Experiment Package (HEPP) is designed to provide a flight evaluation system for low temperature heat pipes. The HEPP will be flown aboard the Long Duration Exposure Facility which will be launched and retrieved as part of the Space Shuttle program. The experiment contains two heat pipes: an axially grooved fixed conductance heat pipe and a liquid blockage thermal diode. A phase change material canister is also integrated with a radiant cooler system. Additional hardware consists of supporting electrical equipment, including electronics for signal conditioning and command functions, a data recorder, and a hermetically sealed battery which powers the experiment. A thermal model was developed to simulate the behavior of the HEPP and a ground test program was conducted to verify the predicted performance of the equipment.
Document ID
19780051725
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Suelau, H. J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Brennan, P. J.
(B & K Engineering, Inc. Towson, Md., United States)
Mcintosh, R.
(NASA Goddard Space Flight Center Systems Div., Greenbelt, Md., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 78-459
Meeting Information
Meeting: International Heat Pipe Conference
Location: Palo Alto, CA
Start Date: May 22, 1978
End Date: May 24, 1978
Accession Number
78A35634
Distribution Limits
Public
Copyright
Other

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