Accession Number:

AD0862908

Title:

Altitude Simulation by Test Facility 1-42B During Repeated Start-Stop Operation of a Rocket Motor

Descriptive Note:

Technical rept.

Corporate Author:

AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA

Personal Author(s):

Report Date:

1969-07-01

Pagination or Media Count:

13.0

Abstract:

One rocket motor assembly was successfully fired and extinguished repeatedly in the low-pressure environment of Vertical Test Cell 1-42B at pressure altitudes of 98,000 to 105,000 feet which demonstrated the capability of this design of propulsion system to start-stop on command in the space environment.

Subject Categories:

  • Solid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE