NASA NTRS · 19650004965
A radial, diaphragm-separated injection method for variable thrust liquid rocket engines with or without mixture ratio variation <eine radiale, membrangetrennte einspritzmethode fur flussigkeitsraketentriebwerke mit variablem schub und/oder variable
Abstract
Radial, diaphragm separated injection method for variable thrust liquid rocket engines with or without mixture ratio variation
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Kayser, L. T.. 1968-12-01. A radial, diaphragm-separated injection method for variable thrust liquid rocket engines with or without mixture ratio variation <eine radiale, membrangetrennte einspritzmethode fur flussigkeitsraketentriebwerke mit variablem schub und/oder variable. https://ntrs.nasa.gov/citations/19650004965
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