Accession Number : AD0852237

Title :   Factory Acceptance Testing of Missile 18F.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date : 19 SEP 1961

Pagination or Media Count : 32

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 : Surface-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE