NASA NTRS · 19680008657
Exploring in aerospace rocketry. 7 - Liquid propellant rocket systems
Abstract
Operating characteristics and design aspects of injector, combustion chamber, and exhaust nozzle for bipropellant rockets
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Conrad, E. W.. 1968-01-01. Exploring in aerospace rocketry. 7 - Liquid propellant rocket systems. https://ntrs.nasa.gov/citations/19680008657
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