Accession Number:

ADA071402

Title:

LGM-30B, Stage II Dissected Motors.

Descriptive Note:

Semi-annual test rept.,

Corporate Author:

OGDEN AIR LOGISTICS CENTER HILL AFB UTAH PROPELLANT LAB SECTION

Personal Author(s):

Report Date:

1979-03-01

Pagination or Media Count:

144.0

Abstract:

This report contains test data from propellant and case bond materials from Minuteman Stage II dissected motors. Testing was performed in accordance with Service Engineering General Test Directive GTD-1 Dissect dated 28 June 1974 and Project M83248C. Statistical analysis includes data from both inner ANP 2864 and outer ANP 2862 propellant. Test smaples were obtained from two dissected motors this test period. Data obtained from these two motors have been combined with earlier test data from these same two motors and from a third motor. Linear regression plots using unique symbols to identify the three motors were used to indicate trends. Most of the propellant specimens were prepared and tested in the axial orientation, that is, parallel to the longitudinal axis of the motor. Author

Subject Categories:

  • Surface-Launched Guided Missiles
  • Solid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE