Accession Number : AD0829594

Title :   MISSILE A-16 TELEMETERING CONFIGURATION AS OF 3 JUNE 1958,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Morehead, D. L.

Report Date : 09 JUN 1958

Pagination or Media Count : 6

Abstract : The report presents those changes in the telemetering configuration of missile A-16 which have occurred since publication of reference (a). Reference (a), when corrected in accordance with the changes here presented, will show the telemetering instrumentation configuration of missile A-16 at the beginning of launch countdown. (Author)

Descriptors :   *TELEMETER SYSTEMS), (*SURFACE TO SURFACE MISSILES, GROUND SUPPORT EQUIPMENT, INSTRUMENTATION, MODIFICATION KITS, CHECKOUT PROCEDURES, FAILURE, TURBOPUMPS, PROPELLANT TANKS, TURBOJET EXHAUST NOZZLES, VERNIER ROCKET ENGINES, FLIGHT CONTROL SYSTEMS, FEEDBACK, GYRO STABILIZERS, YAW, PITCH(MOTION), HEAT TRANSFER, CALORIMETRY, THERMOCOUPLES.

Subject Categories : Surface-launched Guided Missiles
      Telemetry

Distribution Statement : APPROVED FOR PUBLIC RELEASE