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Long Duration Exposure Facility (LDEF) low-temperature Heat Pipe Experiment Package (HEPP) flight resultsThe Low Temperature Heat Pipe Flight Experiment (HEPP) is a fairly complicated thermal control experiment that was designed to evaluate the performance of two different low temperature ethane heat pipes and a n-Heptane Phase Change Material (PCM) canister. A total of 388 days of continuous operation with an axially grooved aluminum fixed conductance heat pipe of axially grooved stainless steel heat pipe diode was demonstrated before the EDS batteries lost power. The inability of the HEPP's radiator to cool below 190 K in flight prevented freezing of the PCM and the opportunity to conduct transport tests with the heat pipes. Post flight tests showed that the heat pipes and the PCM are still functioning. This paper presents a summary of the flight data analysis for the HEPP and its related support systems. Pre and post-flight thermal vacuum tests results are presented for the HEPP thermal control system along with individual heat pipe performance and PCM behavior. Appropriate SIG related systems data will also be included along with a 'lessons learned' summary.
Document ID
19920018074
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcintosh, Roy
(California Inst. of Tech. Pasadena., United States)
Mccreight, Craig
(California Inst. of Tech. Pasadena., United States)
Brennan, Patrick J.
(OAO Corp. Greenbelt, MD., United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1992
Publication Information
Publication: NASA. Langley Research Center, Second LDEF Post-Retrieval Symposium Abstracts
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
92N27317
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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