Propellant Surveillance Report LGM-30 A & B Stage I, TP-H1011.
OGDEN AIR LOGISTICS CENTER HILL AFB UT PROPELLANT ANALYSIS LAB
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This report contains propellant test results from cartons of TP-1011 bulk propellant representing LGM-30 A and B First Stage Minuteman Motors. Testing was accomplished in accordance with MMWRBM Project M04046C-WNL01529. The purpose of testing was to determine and provide early warning of any serious degradation trends occurring in the propellant for service life predictions. An analysis of all parameters indicates that no potential problems are expected in the propellant for at least two years past the oldest data point. Data stored in the G085 System were plotted utilizing the IBM 360-65 Computer and CAL-COMP Plotter. The data range at any age can be found by suitable inquiry of the G085 System. Each point on the regression plot represents the mean of all samples at that particular age. The number of specimens at each point is indicated on the sample size summary sheet accompanying each regression plot or group of regression plots. Author
- Surface-Launched Guided Missiles
- Solid Propellant Rocket Engines
- Solid Rocket Propellants