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)


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    Title :

    Flight Test Design for the Survivable Radio Guidance System


    Publication date :

    1969


    Size :

    206 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English