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Orbiter thermal control subsystem developmentSelected major hardware components and subsystems of the shuttle orbiter are described. These include the hardware configurations, development problems and solutions, performance requirements and attainment, major hardware fabrication problems and solutions, development test objectives and implementation, and utilization of test results for hardware refinements. The subsystems selected for discussion are the space radiator, the ammonia boiler, the flash evaporator, and avionics cold plates.
Document ID
19790023113
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Laubach, G. E. (Rockwell International Corp. Downey, CA, United States)
Date Acquired
August 9, 2013
Publication Date
October 1, 1978
Publication Information
Publication: ESA Spacecraft Thermal and Environ. Control Systems
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
79N31284
Funding Number(s)
CONTRACT_GRANT: NAS9-14000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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