NASA NTRS · 19650025799
Flow system startup of a full-scale simulated nuclear rocket engine
Abstract
Performance of liquid hydrogen flow system during startup transient of nuclear rocket in full scale simulated engine system
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Colmery, B. H., Powers, A. G.. 1965-01-01. Flow system startup of a full-scale simulated nuclear rocket engine. https://ntrs.nasa.gov/citations/19650025799
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