Factory Acceptance Testing of Missile 44F 27-0012-7B.
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
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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
- Surface-Launched Guided Missiles