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; Propellant utilization system; and Propulsion system. (Author)
Factory Acceptance Testing of Missile 141D
1961
35 pages
Report
No indication
English
Factory Acceptance Testing of Missile 40E
NTIS | 1961
Factory Acceptance Testing of Missile 46E
NTIS | 1961
Factory Acceptance Testing of Missile 3F
NTIS | 1961
Factory Acceptance Testing of Missile 10F
NTIS | 1961
Factory Acceptance Testing of Missile 36E
NTIS | 1961