Accession Number:

AD0862053

Title:

Evaluation of a Platform Vertical Single-Component Thrust Stand

Descriptive Note:

Technical rept.

Corporate Author:

AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA

Personal Author(s):

Report Date:

1969-09-01

Pagination or Media Count:

23.0

Abstract:

This report describes the calibration of a platform vertical 6- component Rocketdyne Rocket Motor Thrust Stand located on Pad 2, Air Force Rocket Propulsion Laboratory, Solid Test Area 1-32. Six-component thrust mmeasurement is possible, but presently the stand is used to measure only the axial component of thrust.

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Solid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE