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Accession Number:
AD0852742
Title:
Factory Acceptance Testing of Missile 37F 27-0012-71.
Corporate Author:
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Report Date:
1961-11-30
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 Inertial guidance system Propellant utilization system and Propulsion system. Author
Pages:
0033
File Size:
0.00MB
