Accession Number : AD0829104

Title :   FACTORY ACCEPTANCE TESTING OF MISSILE 130D.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date : 15 MAR 1963

Pagination or Media Count : 88

Abstract : This report presents the results of composite tests, Project Mercury, conducted 7 March 1963, and subsequent post-composite testing. Pertinent systems level testing is also included. Final acceptance of Missile 130D was based on successful performance of all missile systems in accordance with Missile Composite Checkout Procedure, and Missile Factory Acceptance Test Plan and Test Evaluation. Before conducting the missile composite checkout, successful performance of each individual system installed on the missile must be determined. (Author)

Descriptors :   (*SURFACE TO SURFACE MISSILES, OPERATIONAL READINESS), ABORT, DETECTORS, ELECTRICAL EQUIPMENT, FLIGHT CONTROL SYSTEMS, PROPELLANT CONTROL, LIQUID ROCKET PROPELLANTS, LIQUID PROPELLANT ROCKET ENGINES, COMMAND AND CONTROL SYSTEMS, GUIDED MISSILE RANGES, TELEMETER SYSTEMS, VERNIER ROCKET ENGINES, IGNITION SYSTEMS, SAFETY, INERTIAL GUIDANCE.

Subject Categories : Surface-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE