The motor ignited and performed satisfactorily in all parameters throughout action time. All required parameters were within the limits prescribed by the Wing VI Operational model Specification, S-133-1001-0-3. Post-test inspection indicated satisfactory performance of all motor components. (Author)
Individual Motor Report M55A1 Minuteman Operational Quality Assurance Rocket Motor QA-1206, 0013837
1973
92 pages
Report
No indication
English
Rocket Engines & Motors , Missile Technology , Booster rockets , Solid propellant rocket engines , Surface to surface missiles , Captive tests , Quality control , Reliability , Thrust vector control systems , Rocket nozzles , Ignition , Thrust , Specific impulse , Graphite , Nozzle inserts , Thermal insulation , Rings , Rocket engine cases , Visual inspection , Performance(Engineering) , M-55a1 motors , Minuteman , M-55 motors
EVOLUTION OF AN AGING PROGRAM - MINUTEMAN STAGE II SOLID ROCKET MOTOR
British Library Conference Proceedings | 1990
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