Paper describes process of applying approved U S Air Force system engineering methodology for incorporating crew performance as essential element of TOTAL system design of manned satellite to achieve optimum system effectiveness; example used is that of identifying, defining, designing, developing and testing crew performance of in-space maintenance tasks as integral aspect of manned satellite research and development program.
Integrating crew performance into space vehicle system design for optimum reliability
Am Astronautical Soc -- Science Technology Ser
Manned Space Reliability Symposium ; 1964 Reliability
1964
19 pages
Conference paper
English
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