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)
Flight Test Design for the Survivable Radio Guidance System
1969
206 pages
Report
Keine Angabe
Englisch
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