NASA NTRS · 19690054783
Space storable propellant performance with the coaxial injector.
Abstract
Space storable hydrocarbon fuel blended FLOX propellant performance with coaxial injector including characteristic velocity, chamber geometry, pressure and heat flux distribution
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Mageean, J. V.. 1969-06-01. Space storable propellant performance with the coaxial injector.. https://ntrs.nasa.gov/citations/19690054783
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