Accession Number : AD0374220

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

Descriptive Note : Quarterly rept. no. 4, 1 Apr-30 Jun 66,

Corporate Author : AEROJET-GENERAL CORP SACRAMENTO CALIF

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

Report Date : JUL 1966

Pagination or Media Count : 92

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, *CONTROLLABLE-THRUST ROCKET MOTORS), RESEARCH MANAGEMENT, DESIGN, SOLID ROCKET PROPELLANTS, CAPTIVE TESTS, PERFORMANCE(ENGINEERING), HIGH ALTITUDE, SIMULATION, ROCKET COMPONENTS, FEASIBILITY STUDIES, PRESSURE, FEEDBACK, TEST EQUIPMENT, DIFFUSERS, CONTROL SYSTEMS (U) BAROMETRIC PRESSURE, SPECIFIC IMPULSE, INTERIOR BALLISTICS, MECHANICAL PROPERTIES, THERMAL PROPERTIES, COMBUSTION CHAMBERS, VARIABLE AREA NOZZLES, BURNING RATE, ROCKET NOZZLES, PLUG NOZZLES, THERMAL INSULATION

Subject Categories : Solid Propellant Rocket Engines
      Solid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE