NASA NTRS · 19840023203
Preliminary engineering report for design of a subscale ejector/diffuser system for high expansion ratio space engine testing
Abstract
The design of a subscale jet engine driven ejector/diffuser system is examined. Analytical results and preliminary design drawings and plans are included. Previously developed performance prediction techniques are verified. A safety analysis is performed to determine the mechanism for detonation suppression.
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Wojciechowski, C. J., Kurzius, S. C., Doktor, M. F.. 1984-04-01. Preliminary engineering report for design of a subscale ejector/diffuser system for high expansion ratio space engine testing. https://ntrs.nasa.gov/citations/19840023203
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