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Accession Number:
AD0852233
Title:
Factory Acceptance Testing of Missile 118D.
Corporate Author:
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Report Date:
1961-07-28
Abstract:
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
Pages:
0053
File Size:
0.00MB
