Accession Number:

AD0902308

Title:

75-LBF PBPS Monopropellant Engine Test and Evaluation.

Descriptive Note:

Final rept. May-Nov 70,

Corporate Author:

AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA

Personal Author(s):

Report Date:

1972-07-01

Pagination or Media Count:

74.0

Abstract:

Two 75-lbf thrust monopropellant hydrazine engines were tested and evaluated to determine the suitability of the hardware for meeting initial PBPS design requirements. One of the engines exceeded all of the minimum specified design and operating requirements with a delivered vacuum thrust in excess of 72 lbf and a specific impulse in excess of 224 seconds for the complete design life of 500 seconds.

Subject Categories:

  • Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE