NASA NTRS · 19630022693
SCALE MODEL TESTING OF 90 DEG TURN EJECTOR SYSTEMS FOR ROCKET ENGINE ALTITUDE SIMULATION
Abstract
Scale model testing of 90 degree turn ejector systems for rocket engine altitude simulation
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Mandell, B., Mc Farland, B. L., Nelson, R. E., Patmor, G. O.. 1963-06-20. SCALE MODEL TESTING OF 90 DEG TURN EJECTOR SYSTEMS FOR ROCKET ENGINE ALTITUDE SIMULATION. https://ntrs.nasa.gov/citations/19630022693
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