Accession Number : AD0379695

Title :   SMALL HIGH PERFORMANCE INTERCEPTOR RESEARCH.

Corporate Author : BOEING CO SEATTLE WASH

Report Date : 10 FEB 1967

Pagination or Media Count : 196

Abstract : This document summarizes results of the 1966 High Performance Interceptor research program. The objective of this program was to develop the techniques and design data which would allow development of high acceleration interceptors. Major areas of investigation include high-g solid propulsion, high response attitude control methods, high-g, high angle-of-attack aerodynamics, and methods of determining integrated missile effectiveness. Summaries of the work accomplished and results obtained in each area are presented along with reference to the formal documentation covering each area. (Author)

Descriptors :   (*ROCKET ENGINES, INTERCEPTION), DESIGN, PERFORMANCE(ENGINEERING) (U) *ANTIMISSILE DEFENSE SYSTEMS, *SURFACE TO AIR MISSILES, *SOLID PROPELLANT ROCKET ENGINES, ACCELERATION, INTERCEPTION PROBABILITIES, ATTITUDE CONTROL SYSTEMS, RESPONSE, FLIGHT CONTROL SYSTEMS, MISS DISTANCE, SIMULATION, MANEUVERABILITY, AERODYNAMIC CONFIGURATIONS, AERODYNAMIC CHARACTERISTICS, IGNITION, SUPERSONIC COMBUSTION, SUPERSONIC COMBUSTION RAMJET ENGINES, ROCKET PROPELLANT GRAINS, AUTOMATIC PILOTS, SECONDARY INJECTION, THRUST VECTOR CONTROL SYSTEMS

Subject Categories : Antimissile Defense Systems
      Surface-launched Guided Missiles
      Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE