Accession Number:

ADA012200

Title:

Preliminary Flight Rating Tests of the HAST Propulsion System

Descriptive Note:

Final rept. Jun 1972-Dec 1973

Corporate Author:

AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA

Personal Author(s):

Report Date:

1975-01-01

Pagination or Media Count:

199.0

Abstract:

Preliminary Flight Rating Tests of the hybrid rocket propulsion system for the HAST target missile were accomplished by the Air Force Rocket Propulsion Laboratory. Nine tests of the flight configuration system were conducted at simulated altitude. Overall operating characteristics and performance were shown to be satisfactory for missile flight tests.

Subject Categories:

  • Guided Missiles
  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE