Design procedures for combustion termination by nozzle area variation.
COATES, R. L., POLZIEN, R. E. /LOCKHEED AIRCRAFT CORP., LOCKHEED PROPULSION CO., ENGINEERING BRANCH, REDLANDS, CALI, PRICE, C. F. /LOCKHEED AIRCRAFT CORP., LOCKHEED PROPULSION CO., ENGINEERING RESEARCH DEPT., REDLANDS
JOURNAL OF SPACECRAFT AND ROCKETS ; 3 , 3 ; 419-425
1966-01-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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