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