Accession Number : AD0852231
Title : Factory Acceptance Testing of Missile 27F.
Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Report Date : 31 OCT 1961
Pagination or Media Count : 33
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)
Descriptors : (*SURFACE TO SURFACE MISSILES, CHECKOUT PROCEDURES), ELECTRICAL EQUIPMENT, FLIGHT CONTROL SYSTEMS, INERTIAL GUIDANCE, LIQUID ROCKET PROPELLANTS, LIQUID PROPELLANT ROCKET ENGINES.
Subject Categories : Air- and Space-launched Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE