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; Inertial guidance system; Propellant utilization system; and Propulsion system. (Author)
Factory Acceptance Testing of Missile 18F
1961
32 pages
Report
No indication
English
Factory Acceptance Testing of Missile 51E
NTIS | 1965
Factory Acceptance Testing of Missile 14F
NTIS | 1961
Factory Acceptance Testing of Missile 48E
NTIS | 1961
Factory Acceptance Testing of Missile 34E
NTIS | 1961
Factory Acceptance Testing of Missile 54E
NTIS | 1961