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At least 1,117 records · Page 62

Rationale for proposed flying-qualities specifications

The NASA Flight Research Center is reviewing the applicability of flying qualities experience to the shuttle mission for the purpose of preparing a shuttle flying qualities specification. This paper is a progress report on this review; the results presented are, of course, preliminary.

Euclid C Holleman↗

High specific impulse gas-core reactors

Calculated estimates of gas core nuclear rocket engine weights for specific impulses ranging from 3000 to 7000 seconds and for engine thrusts ranging from 4400 to 440,000 newtons

Ragsdale, R. G.↗