Accession Number:

AD0862052

Title:

Flexible Exit Cone Nozzle Demonstration Firing Results

Descriptive Note:

Test rept.

Corporate Author:

AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA

Personal Author(s):

Report Date:

1969-08-01

Pagination or Media Count:

24.0

Abstract:

This report describes the test firing of a thrust vector control system TVC on the AFRPL 40-inch-diameter Char Motor. The TVC system consisted of a movable exit cone Flex-X nozzle and support hardware, which was designed to combine the advantages of the elastomeric seal with those of the supersonic split-line nozzle.

Subject Categories:

  • Solid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE