Accession Number : AD0371449
Title : INVESTIGATION OF ADVANCED RAMJETS IN AIR-TO-SURFACE MISSIONS.
Descriptive Note : Technical publication,
Corporate Author : NAVAL ORDNANCE TEST STATION CHINA LAKE CALIF
Personal Author(s) : Traver ,R. H. ; Porter,H. O.
Report Date : APR 1965
Pagination or Media Count : 114
Abstract : The attributes of the low-volume ramjet and the solid-fuel ramjet engines were analyzed. The analysis considered the application of these ramjet engine concepts to the ARM 1 and ARM 2 air-to-surface antiradar missiles. Optimum ramjet engine designs were developed for each. Comparative missile designs utilizing both solid and liquid propellant rocket engines were made. Computer simulation programs were developed for each missile and propulsion combination. The mission performance of each was then determined by simulating typical attack trajectories. The results showed that the low-volume ramjet achieved, by a wide margin, the longest usable range in both missile systems. The solid-fuel ramjet failed by a significant margin to match the range performance of comparative rocket systems. (Author)
Descriptors : (*RAMJET ENGINES, AIR-TO-SURFACE) (U) SOLID JET ENGINE FUELS, AIR TO SURFACE MISSILES, OPTIMIZATION, DESIGN, SOLID PROPELLANT ROCKET ENGINES, LIQUID PROPELLANT ROCKET ENGINES, SIMULATION, COMPUTER PROGRAMMING, DESCENT TRAJECTORIES, RANGE(DISTANCE), AERODYNAMIC CHARACTERISTICS, PROPENES, OXIDES, LEVEL FLIGHT, CLIMBING, HIGH ALTITUDE, LOW ALTITUDE, BOOSTER ROCKETS
Subject Categories : Air- and Space-launched Guided Missiles
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE