Accession Number : AD0374220

Title :   FEASIBILITY DEMONSTRATION OF A SINGLE-CHAMBER CONTROLLABLE SOLID ROCKET MOTOR

Descriptive Note : Quarterly rept. no. 4, 1 Apr-30 Jun 1966

Corporate Author : AEROJET-GENERAL CORP SACRAMENTO CA

Personal Author(s) : Levinsky, Charles T ; Kobalter, Gerald F

PDF Url : AD0374220

Report Date : Jul 1966

Pagination or Media Count : 105

Abstract : The heavyweight motor development, the lightweight motor design and the propellant re-evaluation were completed. The final heavyweight motor test results are presented along with the data plots and photographs. The motor was fired at simulated altitude and successfully extinguished.

Descriptors :   *SOLID PROPELLANT ROCKET ENGINES, BURNING RATE, CAPTIVE TESTS, COMBUSTION CHAMBERS, DIFFUSERS, FEASIBILITY STUDIES, FEEDBACK, HIGH ALTITUDE, INTERIOR BALLISTICS, MECHANICAL PROPERTIES, PERFORMANCE(ENGINEERING), PLUG NOZZLES, PRESSURE, RESEARCH MANAGEMENT, ROCKET COMPONENTS, ROCKET NOZZLES, SIMULATION, SOLID ROCKET PROPELLANTS, SPECIFIC IMPULSE, TEST EQUIPMENT, THERMAL INSULATION, THERMAL PROPERTIES, VARIABLE AREA NOZZLES

Subject Categories : Solid Propellant Rocket Engines
      Solid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE