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: Abort sensing and implementation system; Azusa system; Electrical system; Flight control system; Guidance system; Propellant utilization system; Propulsion system; Range safety command system; and Telemetry system. (Author)
Factory Acceptance Testing of Missile 93D
1961
91 pages
Report
Keine Angabe
Englisch
Missile Technology , Surface to surface missiles , Checkout procedures , Guided missile safety , Abort , Guided missile tracking systems , Flight control systems , Radio beacons , Liquid rocket propellants , Liquid propellant rocket engines , Telemeter systems , Electrical equipment , Atlas , Azusa , Xsm-65d missiles
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