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Development of a thermal diode heat pipe for cryogenic applicationsThe paper describes the development of a cryogenic thermal diode heat pipe for space flight applications. The diode has ethane working fluid, and uses the liquid blockage technique with an internal blocking orifice, to accomplish shutoff in the reverse mode. The pipe is 0.635 cm OD by 75.82 cm long including a 2.54 cc excess liquid reservoir. Experimental data are presented for forward mode throughput vs tilt, film coefficients, and reverse mode characteristics. Transport capacity is 1000 w-cm at 2.5 cm tilt. Evaporator and condenser film coefficients were 0.92 and 1.64 w/sq cm K, respectively.
Document ID
19770037036
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Quadrini, J. A.
(Grumman Aerospace Corp. Bethpage, N.Y., United States)
Mccreight, C. R.
(NASA Ames Research Center Technology Development Branch, Moffett Field, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 77-192
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Los Angeles, CA
Start Date: January 24, 1977
End Date: January 26, 1977
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
77A19888
Funding Number(s)
CONTRACT_GRANT: NAS2-7492
Distribution Limits
Public
Copyright
Other

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