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 Soc Automotive Engrs -- Paper n 48A for meeting Apr 8-11 1958 15 p)
Turbine engines for high speed missiles
SAE -- J
Society of Automotive Engineers -- Journal ; 66 , n 7
1958
3 pages
Article (Journal)
English
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Turbine engines for high speed missiles
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