Accession Number : ADA198854

Title :   LGM-30B Stage II Dissected Motor Test Report.

Descriptive Note : Annual rept. 1 Jan-31 Dec 88,

Corporate Author : OGDEN AIR LOGISTICS CENTER HILL AFB UT PROPELLANT ANALYSIS LAB

Personal Author(s) : Dalaba, Elizabeth M.

Report Date : JUN 1988

Pagination or Media Count : 141

Abstract : This report contains data from second time testing of a dissected Minuteman II Stage II motor, S/N 0022123. Statistical statements are based on F and student t tests. Data have been shown on multi-regression plots for reference only. These plots show the position of the current data relative to the prior testing of this motor and other motors. Plots have been made to show differences between blocks and slices of propellant, both unconditioned and conditioned. There are unexplained differences between the two test periods, as well as differences between conditioned and unconditioned specimens. Keywords: Dissected motor, Solid propellant, Minuteman, Surface to surface missiles. (jhd)

Descriptors :   *SOLID PROPELLANTS, *SOLID PROPELLANT ROCKET ENGINES, MOTORS, SURFACE TO SURFACE MISSILES, STATISTICAL TESTS, DISSECTION.

Subject Categories : Liquid Propellant Rocket Engines
      Liquid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE