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Pressure control and analysis report: Hydrogen Thermal Test Article (HTTA)

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Abstract

Tasks accomplished during the HTTA Program study period included: (1) performance of a literature review to provide system guidelines; (2) development of analytical procedures needed to predict system performance; (3) design and analysis of the HTTA pressurization system considering (a) future utilization of results in the design of a spacecraft maneuvering system propellant package, (b) ease of control and operation, (c) system safety, and (d) hardware cost; and (4) making conclusions and recommendations for systems design

Topics: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
Year: 1971
OAI identifier: oai:casi.ntrs.nasa.gov:19760015192

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