Transient pressure drop and heat transfer characteristics of regeneratively cooled nozzle assembly used in full scale, cold flow nuclear rocket test facility
Cooldown characteristics of regenerative nozzle used in full-scale, cold-flow, nuclear rocket test facility
1967-05-01
Sonstige
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Englisch
Cooldown requirements for nuclear rocket missions.
AIAA | 1967
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AIAA | 1991
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