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Test results of a pumped two-phase mounting plate with ammoniaThe design, fabrication, and testing of full-scale prototype units of a two-phase mounting plate (TPMP), which will be used in a two-phase ammonia-based thermal control system for a large spacecraft, are described. The mounting plate uses an evaporator design in which liquid is mechanically pumped through porous feed tubes within the plate. The prototype TPMPs were tested with ammonia at heat loads over 3000 W (3.2 W/sq cm) and local heat fluxes of up to 4 W/sq cm. Calculated total heat transfer coefficients from these tests were between 0.8 and 1.0 W/sq cm per C. This represents a better than twenty-fold improvement over comparable single-phase heat transfer coefficients. Design diagrams are included.
Document ID
19870035123
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Swanson, T. D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Mccabe, M. E., Jr.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Grote, M. G.
(McDonnell Douglas Astronautics Co. Saint Louis, MO, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 87-0075
Accession Number
87A22397
Distribution Limits
Public
Copyright
Other

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