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Instrument canister thermal controlA transient thermal analysis and test of a thermal control canister is described. The 1 x 1 x 3 m canister provides a uniform thermal environment for shuttle instrument payloads requiring fine temperature control, the design goal being operation between 0 C and 20 C with a range of plus or minus 1 C at any selected set-point temperature. The canister side walls are isothermalized by a system of longitudinal and circumferential heat pipes rejecting heat through feedback controlled, variable conductance heat pipes to side mounted radiators. A breadboard model of two side walls and two radiators was tested in a thermal vacuum chamber. The breadboard was stable over a wide range of effective environments, experiment dissipations, and control point temperature levels.
Document ID
19770054420
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Harwell, W.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Haslett, R.
(Grumman Aerospace Corp. Bethpage, N.Y., United States)
Ollendorf, S.
(NASA Goddard Space Flight Center Greenbelt, Md., United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1977
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 77-761
Meeting Information
Meeting: Thermophysics Conference
Location: Albuquerque, NM
Start Date: June 27, 1977
End Date: June 29, 1977
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
77A37272
Distribution Limits
Public
Copyright
Other

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