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: Electrical system; Flight control system; Guidance system; Instrumentation range safety system; Propellant utilization system; and Propulsion system. (Author)
Factory Acceptance Testing of Missile 118D
1961
53 pages
Report
No indication
English
Atlas/Agena Flight Test Directive Atlas Missile 118D
NTIS | 1962
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