Accession Number : AD0833326

Title :   XSM-65D AUTOPILOT SYSTEM ACCEPTANCE TEST PLAN,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Burgett, F. C.

Report Date : 18 SEP 1959

Pagination or Media Count : 26

Abstract : The primary objective of the system acceptance test is to establish that the missileborne autopilot system operates satisfactorily by acceptable authorized drawings, specifications and reports. (Author)

Descriptors :   *AUTOMATIC PILOTS), (*SURFACE TO SURFACE MISSILES, FLIGHT CONTROL SYSTEMS, PERFORMANCE(ENGINEERING), INERTIAL GUIDANCE, HYDRAULIC SERVOMECHANISMS, GYRO STABILIZERS, CALIBRATION, TORQUE, HYDRAULIC ACTUATORS, SIGNAL GENERATORS, MONITORS, RECORDING SYSTEMS, RELIABILITY, VOLTAGE, FREQUENCY, RESPONSE.

Subject Categories : Surface-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE