Accession Number : AD0866484
Title : Ramjet Engine Design Study for Sandpiper Target Drone.
Descriptive Note : Final rept. 1 Apr-1 Oct 69,
Corporate Author : MARQUARDT CO VAN NUYS CA
Personal Author(s) : Carlson, Charles H.
Report Date : FEB 1970
Pagination or Media Count : 120
Abstract : Advanced target drones will require increased performance and time-on-station to provide adequate simulation of future airborne threats. To be operationally attractive these units should provide realistic simulation over a broad operating envelope, have a low initial cost, and be capable of recovery and reuse. The normal shock inlet ramjet as exemplified by the technology obtained in the surface launched Redhead/Roadrunner Target Drone Program (U.S. Army Contract DA-01-021-AML-10991 Z) appears to be particularly well suited to this requirement. This report presents the results of a design study undertaken to define an optimum ramjet engine size for the air launched Advanced Sandpiper Target Drone. The report also describes a minimum time and cost exploratory development program providing a ground test demonstration of the engine capabilities. (Author)
Descriptors : (*GUIDED MISSILE TARGETS, RAMJET ENGINES), (*RAMJET ENGINES, DESIGN), OPTIMIZATION, PLANNING, MISSION PROFILES, AERODYNAMIC CHARACTERISTICS, PROPELLANT CONTROL, FUEL CONSUMPTION, THERMAL ANALYSIS, FLIGHT TESTING.
Subject Categories : Guided Missile Launching and Basing Support
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE