NASA NTRS · 19680024882
A hot gas generator for large scale supersonic combustor testing
Abstract
Exhaust gas of hydrazine-nitrogen tetroxide rocket for simulating combustor inlet requirements of scramjet engines
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Lezberg, E. A., Metzler, A. J.. 1968-01-01. A hot gas generator for large scale supersonic combustor testing. https://ntrs.nasa.gov/citations/19680024882
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