Accession Number : AD0781211
Title : Propellant Surveillance Report, LGM-30 F and G, Stage 1, Phase A, Series IV, TP-H1011.
Descriptive Note : Semi-annual,
Corporate Author : OGDEN AIR MATERIEL AREA HILL AFB UTAH PROPELLANT LAB SECTION
Personal Author(s) : Thompson,John A.
Report Date : MAR 1974
Pagination or Media Count : 192
Abstract : The report contains propellant test results from cartons of TP-H1011 bulk propellant representing LGM-30 F and G First Stage Minuteman Motors. This report uses a statistical approach to analyze the bulk carton propellant. An analysis of all parameters indicates that eight years of aging at 77F temperature has not greatly affected the properties of the propellant. No potential problems are expected in the propellant for at least two years past the oldest data point. Each point on the regression plot represents all samples at that particular age. The number of samples at each point is indicated on the sample size summary sheet on the page accompanying each regression plot. The data range at any age can be found by suitable inquiry of the GO85 system. (Author)
Descriptors : *Surface to surface missiles, *Solid propellant rocket engines, *Solid rocket propellants, *Aging(Materials), Tensile stress, Stress strain relations, Rupture, Regression analysis
Subject Categories : Surface-launched Guided Missiles
Solid Propellant Rocket Engines
Solid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE