Accession Number : AD0860328

Title :   Flight Test Design for the Survivable Radio Guidance System.

Descriptive Note : Final technical rept. Jul 68-Jul 69.

Corporate Author : GENERAL ELECTRIC CO SYRACUSE NY HEAVY MILITARY ELECTRONIC SYSTEMS

Report Date : OCT 1969

Pagination or Media Count : 206

Abstract : The technical documentary report describes the result of a program of flight test planning for an advanced radio guidance system intended for missile applications. The purpose of the flight test is to evaluate key technologies of the system concept; the specific test objectives are the following: Evaluation of the trajectory estimation accuracy of the system; Evaluation of the flightworthiness of the rubidium frequency standard which would be part of the missileborne equipment; Evaluation of the acquisition capability of the narrow-bandwidth computer-designated receiver which would be used in the system. (Author)

Descriptors :   *TERMINAL GUIDANCE), (*GUIDED MISSILES, (*POSITION FINDING, DOPPLER SYSTEMS), GUIDED MISSILE TRAJECTORIES, ORBITS, RADIO EQUIPMENT, ATOMIC CLOCKS, RUBIDIUM, STANDARDS, ACCURACY.

Subject Categories : Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE