Flexible Exit Cone Nozzle Development Program.

Abstract

This program was initiated by the Air Force Rocket Propulsion Laboratory to demonstrate the flexible exit cone omniaxis movable nozzle concept by rocket motor testing. Program objectives are as follows: develop flexible exit cone design and criteria, perform a TVC system comparison, and demonstrate the flexible exit cone nozzle performance on four AFRPL 36 in. diameter char motor static tests with vectoring. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 01, 1971
Accession Number
AD0884845

Entities

People

  • Jonathan W. Wilson

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Captive Tests
  • Diameters
  • Movable Nozzles
  • Nozzles
  • Rocket Engines
  • Rocket Propulsion
  • Rockets
  • Static Tests
  • Test Methods

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Electrical Engineering
  • Systems Analysis and Design