Accession Number : AD0851391

Title :   Control-Rate of Turn, Autopilot CVA Part No. 27-04574-1.

Descriptive Note : Evaluation test rept.,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Fernald, P.

Report Date : 27 MAR 1961

Pagination or Media Count : 58

Abstract : The purpose of the report is to describe the test equipment, test procedure, and results of the evaluation testing of an angular rate gyro.

Descriptors :   (*GYROSCOPES, RELIABILITY(ELECTRONICS)), VIBRATION, HUMIDITY, ACCELERATION, THERMAL SHOCK, AUTOMATIC PILOTS, SURFACE TO SURFACE MISSILES.

Subject Categories : Surface-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE