Accession Number:

AD0884845

Title:

Flexible Exit Cone Nozzle Development Program.

Descriptive Note:

Final rept. Aug 67-May 71,

Corporate Author:

THIOKOL CHEMICAL CORP BRIGHAM CITY UTAH WASATCH DIV

Personal Author(s):

Report Date:

1971-05-01

Pagination or Media Count:

109.0

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

Subject Categories:

  • Rocket Engines
  • Solid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE