Propulsion system of missiles is composite of engine, induction and exhaust system, engine installation, and fuel system; for region of flight within earth's atmosphere and speeds up to Mach 4 air-breathing engines are most efficient for many applications, gas turbine is superior to ramjet or turbojet, ramjet and rocket; high performance can be attained by matching fixed geometry inlet and exhaust system with engine characteristics.
Design and operation of propulsion systems for cruise-type missiles
SAE -- Paper
SAE Meeting ; 1959
1959
7 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
THE DESIGN AND OPERATION OF PROPULSION SYSTEMS FOR CRUISE-TYPE MISSILES
SAE Technical Papers | 1959
|Lithergol Dual Propulsion for Cruise Missiles
NTIS | 1978
|Springer Verlag | 2004
|