Accession Number:

AD0374761

Title:

CELLULAR COMBUSTION CHAMBER PROGRAM (PROJECT SCORPIO). A SIMPLIFIED CLUSTERING TECHNIQUE FOR ROCKET ENGINE MODULES

Descriptive Note:

Final rept. Aug 1963-Nov 1965 on Phase 3

Corporate Author:

AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA

Report Date:

1966-03-01

Pagination or Media Count:

120.0

Abstract:

Results of the tests and evaluations performed on 1 a simplified clustering technique for rocket engine modules, 2 single modules utilizing simplified large thrust per element injectors and film-cooled thrust chambers, and 3 a unique thrust vectoring mechanism known as the CAM Ring Gimbal are presented. The high-energy, cryogenic propellant combination of liquid oxygen and liquid hydrogen was used throughout.

Subject Categories:

  • Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE