FEASIBILITY DEMONSTRATION OF A SINGLE-CHAMBER CONTROLLABLE SOLID ROCKET MOTOR

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.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1966
Accession Number
AD0374220

Entities

People

  • Charles T. Levinsky
  • Gerald F. Kobalter

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Actuators
  • Altitude
  • Burning Rate
  • Combustion
  • Computers
  • Contracts
  • Control Systems
  • Ignition
  • Ignition Systems
  • Materials
  • Materials Processing
  • Measurement
  • Propellants
  • Rocket Engines
  • Test And Evaluation
  • Test Equipment
  • Test Facilities

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Aerospace Test and Evaluation
  • Rocket Propulsion.