NASA NTRS · 19690054755
Hypersonic research engine integrated propulsion control.
Abstract
Integrated propulsion control system for ramjet Hypersonic Research Engine to operate at 3-8 Mach numbers
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Colwill, T., Curran, W., Stiglic, P.. 1969-06-01. Hypersonic research engine integrated propulsion control.. https://ntrs.nasa.gov/citations/19690054755
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