NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Flight data for the Cryogenic Heat Pipe (CRYOHP) ExperimentThis paper presents the flight test results and data correlation for the Cryogenic Heat Pipe Flight Experiment (CRYOHP). CRYOHP is a Hitchhiker Canister experiment that was flown aboard the shuttle Discovery (STS-53) in December of 1992. Two different axially grooved oxygen heat pipes were tested to determine their startup behavior and transport capability in micro-gravity. Three startup cycles were conducted with each heat pipe and transport data was obtained over the range of 60 K to 140 K. Startup in flight was repeatable but slower than observed in ground tests. The transport data shows good agreement with the theoretical model. The CRYOHP test bed, which incorporates five Stifling cycle refrigerators to provide the cryo-cooling, performed as predicted and offers a good micro-gravity test bed for cryogenic thermal devices.
Document ID
19930062491
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brennan, Patrick J.
(OAO Corp. Greenbelt, MD, United States)
Thienel, Lee
(Jackson and Tull Greenbelt, MD, United States)
Swanson, Ted
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Morgan, Michael
(USAF, Wright Lab. Wright-Patterson AFB, OH, United States)
Date Acquired
August 16, 2013
Publication Date
July 1, 1993
Subject Category
Engineering (General)
Report/Patent Number
AIAA PAPER 93-2735
Report Number: AIAA PAPER 93-2735
Meeting Information
Meeting: AIAA, Thermophysics Conference
Location: Orlando, FL
Country: United States
Start Date: July 6, 1993
End Date: July 9, 1993
Sponsors: AIAA
Accession Number
93A46488
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available