Advantages; description of straight turbojet engine and combined turbojet-ramjet engine for flight speeds in vicinity of Mach 4.0; performance at cruise conditions and in acceleration region presented for sample set of assumptions; typical missile applications. (see also abstract in SAE -- J v 66 n 7 July 1958 p 78-80)
Turbine engines for high speed missiles
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1958 Propulsion
1958
15 pages
Aufsatz (Konferenz)
Englisch
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