Integrated propulsion control system for ramjet Hypersonic Research Engine to operate at 3-8 Mach numbers
Hypersonic research engine integrated propulsion control.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE ; 1969 ; COLORADO SPRINGS, COLO.
1969-06-01
Conference paper
No indication
English
Hypersonic research engine integrated propulsion control
AIAA | 1969
|Hypersonic Research Engine Integated Propulsion Control
AIAA | 1971
|Hypersonic propulsion research
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NTIS | 1987
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NTRS | 1990
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