Spacecraft thermal control, NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

NASA/SP-8105, Spacecraft thermal control, NASA SPACE VEHICLE DESIGN CRITERIA (Environment), NASA (Washington, DC, United States), May,1973, pp. 48, Format(s): PDF 2497k

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Guidance for the assessment and control of spacecraft temperatures is provided with emphasis on unmanned spacecraft in the space environment. The heat balance, elements of thermal design,and thermal control are discussed along with thermal testing, design criteria, and recommended practices.

Keywords:	space vehicles, spacecraft design, temperature control, aerospace environments, thermal environments, unmanned spacecraft
CASI Document ID Number:	73N26890
Subjects:	Engineering: Fluid Mechanics and Thermodynamics: Thermal Protection
ID Code:	152
Deposited On:	23 May 2002