Sounding rocket heat pipe experiment.An experiment was conducted during October 1971 aboard a sounding rocket to observe the operation of several heat pipes in a zero gravity environment. The pipe designs which were tested included a spiral artery, a pedestal artery, and a plain groove. Two control pipes without wicking were also flown. The two artery pipes were similar to those which will be used on the OAO-C satellite, while the groove pipe was similar to that used on the ATS-F spacecraft. The results of the experiment indicate that the heat pipes operated satisfactorily during the flight which included four minutes of zero gravity.
Document ID
19720041538
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcintosh, R. (NASA Goddard Space Flight Center Greenbelt, Md., United States)
Knowles, G.
Hembach, R. J. (Grumman Aerospace Corp. Bethpage, N.Y., United States)
Date Acquired
August 6, 2013
Publication Date
April 1, 1972
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 72-259Report Number: AIAA PAPER 72-259
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Thermophysics Conference
Location: San Antonio, TX
Start Date: April 10, 1972
End Date: April 12, 1972
Sponsors: American Institute of Aeronautics and Astronautics