In this part, the state of the art for several propulsion system components is reviewed, and some of the important factors which must be considered during the design of a supersonic propulsion system are pointed out. The discussion will be centered around the Mach number 3 cruise airplane of part III and the multimission airplane of part II.
IV. Air-Breathing Propulsion Systems for Supersonic Aircraft
National Meeting on the Future of Manned Military Aircraft ; 1960 ; San Diego, CA, US
1960-10-01
Miscellaneous
No indication
English