Flow system startup of a full-scale simulated nuclear rocket engine.

Colmery, B. H.; Powers, A. G.

NASA NTRS · 19660033060

Flow system startup of a full-scale simulated nuclear rocket engine.

Colmery, B. H.·Powers, A. G.

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Abstract

Liquid hydrogen flow system startup of full scale simulated nuclear rocket engine

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PROPELLANT TESTING ENGINE TESTING LIQUID HYDROGEN ROCKET ENGINE NUCLEAR PROPULSION

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Colmery, B. H., Powers, A. G.. 1965-10-01. Flow system startup of a full-scale simulated nuclear rocket engine.. https://ntrs.nasa.gov/citations/19660033060

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