Accession Number:

ADA002757

Title:

Propellant Test Results, LGM-30 Stage 3, Dissected Motor Program

Descriptive Note:

Semi-annual rept.

Corporate Author:

OGDEN AIR LOGISTICS CENTER HILL AFB UT PROPELLANT LAB SECTION

Personal Author(s):

Report Date:

1974-10-01

Pagination or Media Count:

190.0

Abstract:

This report contains results of propellant testing of LGM-30 Stage 3 dissected motors. Testing was accomplished in accordance with General Test Directive 3 and MME 74NE102. Data from this test period and from previous test periods have been combined and included in regression analyses. Motors 0031064, 0031134, 0032434, 0033174 and Grain 131 have been combined in composite regressions. In general, data are in agreement with past data. Shore A hardness is an exception. There are some statistically significant trends which are not of immediate concern.

Subject Categories:

  • Surface-Launched Guided Missiles
  • Solid Propellant Rocket Engines
  • Solid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE