Before conducting the missile composite checkout, successful performance of each individual system installed on the missile must be determined. The following is a list of the procedures used for acceptance testing of each system: Atlas optical beacon system; Azusa system; Electrical system; Flight control system; Inertial guidance system; Instrumentation beacon system; Propellant utilization system; Propulsion system; Range safety command system; and Telemetry system. (Author)
Factory Acceptance Testing of Missile 14F
1961
86 pages
Report
No indication
English
Missile Technology , Surface to surface missiles , Checkout procedures , Radio beacons , Guided missile tracking systems , Electrical equipment , Flight control systems , Inertial navigation , Liquid rocket propellants , Liquid propellant rocket engines , Guided missile safety , Telemeter systems , Atlas , Azusa , Xsm-65f missiles
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