Accession Number : AD0830559

Title :   VALIDATION PROCEDURE FOR THE TEST CONDUCTORS LAUNCH CONTROL SYSTEM (ELECTRICAL) 'D' SERIES R AND D SYCAMORE S-1 AND S-2,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Eggert, A. L.

Report Date : 13 AUG 1958

Pagination or Media Count : 24

Abstract : This manual provides instructions for validating the Test Conductors Launch Control System (Electrical) 'D' Series R and D, at the Sycamore S-1 and S-2 Sites. The procedure determines that the electrical control equipment and circuitry of the Test Conductors Launch Control System is functioning correctly and properly connected. (Author)

Descriptors :   *CONTROL SYSTEMS), (*GUIDED MISSILE LAUNCHERS, SURFACE TO SURFACE MISSILES, LAUNCHING SITES, ELECTRICAL EQUIPMENT, GROUND SUPPORT EQUIPMENT, CHECKOUT PROCEDURES, SEQUENCES(MATHEMATICS), ELECTRIC CONNECTORS, INSTRUCTION MANUALS, INDICATOR LIGHTS, MONITORS, CONTROL PANELS, SIMULATION, LIQUID PROPELLANT ROCKET ENGINES.

Subject Categories : Electrical and Electronic Equipment
      Guided Missile Launching and Basing Support
      Surface-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE