Accession Number : AD0829051

Title :   FACTORY ACCEPTANCE TESTING OF MISSILE 109D.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date : 15 NOV 1961

Pagination or Media Count : 93

Abstract : This report presents the results of composite testing and post-composite testing. Pertinent systems level testing is also included. Final acceptance of Project Mercury Missile 109D was based on successful performance of all missile systems in accordance with Missile Composite Checkout Procedure, Revision, and Missile Composite System Che ckout Evaluation Data. 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, SAFETY, INERTIAL GUIDANCE.

Subject Categories : Surface-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE