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Self-regulating heater application to Shuttle/Centaur hydrazine fuel line thermal controlThe Shuttle/Centaur high energy upper stage vehicle thermal environments were more severe than previous Centaur vehicle thermal environments, creating need for a new hydrazine fuel line thermal control technique. Constant power heaters did not satisfy power dissipation requirements, because the power required to maintain fuel line thermal control during cold conditions exceeded the maximum power allowable during hot conditions. Therefore, a Raychem Thermolimit self-regulating heater was selected for this application, and was attached to the hydrazine fuel line with Kapton and aluminum foil tapes. Fuel line/heater thermal modeling and subsequent thermal vacuum chamber testing simulated heater thermal performance during all worst-case Shuttle/Centaur thermal environmental conditions. Fuel line temperatures were maintained between the 4C to 71C limits during all analytical and test cases. Finally, the thermal model predictions were correlated with the test data, thereby ensuring that the model would provide satisfactory predictions for future missions and/or vehicles.
Document ID
19870055807
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Unkrich, David B.
(General Dynamics Corp. Space Systems Div., San Diego, CA, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1987
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 87-1570
Accession Number
87A43081
Funding Number(s)
CONTRACT_GRANT: NAS3-22901
Distribution Limits
Public
Copyright
Other

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