Accession Number:

ADA000449

Title:

Five Pound Bipropellant Engine

Descriptive Note:

Final rept. May 1973-Jul 1974

Corporate Author:

AEROJET LIQUID ROCKET CO SACRAMENTO CA

Personal Author(s):

Report Date:

1974-09-01

Pagination or Media Count:

442.0

Abstract:

A fifteen-month program was conducted to develop and demonstrate the technology required to provide a five-pound thrust bipropellant engine capability for attitude control functions typical of future Air Force requirements. Phase I included detailed studies and trade-off analyses of missionsystem requirements versus engine parametrics. Phase II developed point designs based upon the Phase I analyses and the results of design verification tests. Phase III consisted of the fabrication and demonstration testing of three variants of a basic engine design designated AJ10-181 to representative mission requirements. All contract requirements were met or exceeded.

Subject Categories:

  • Liquid Propellant Rocket Engines
  • Liquid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE