Large scale hydrogen fueled supersonic combustor test at simulated Mach 8 flight, describing fuel injector design
Large scale supersonic combustor testing at conditions simulating Mach 8 flight
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 6TH ; 1970 ; SAN DIEGO, CA
1970-06-01
Conference paper
No indication
English