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    • 11. 发明专利
    • TESTER FOR MISSILE
    • JPH0350500A
    • 1991-03-05
    • JP18434689
    • 1989-07-17
    • NISSAN MOTOR
    • NAKANO TORU
    • F42B15/00F42B35/00G01M99/00G05D1/08
    • PURPOSE:To test the performance under the equivalent conditions to actual launching missile state by bearing-supporting rotatably in a direction of degree of freedoms of the other of body pitching direction and body rolling direction of a missile to a base member a support for bearing-supporting rotatably in a direction of degree of freedoms of one of the body pitching direction and body rolling direction of a missile. CONSTITUTION:A rocket 1 is bearing-supported rotatably in a body rolling direction R through a bearing 12 provided at the end of the body 2 of the rocket 1 and a bearing 13 provided through the position Q of center of gravity of the body 2 to a support 11 of a tester 3. The support 11 itself is bearing- supported rotatably to a leg 10 through a bearing 14 around a pitch axis arranged on an axis l passing the position Q, and the whole rocket 1 supported to the support 11 has degrees of freedoms of rotating in orthogonal axes of the body rolling direction R and body pitching direction P. When the missile is set in the tester and started, the attitude controller of the missile is operated in the same manner as the actual missile launching state to be evaluated for the operation.
    • 13. 发明专利
    • FLYING BODY FOR TEST EVALUATION
    • JPH02166399A
    • 1990-06-27
    • JP31998588
    • 1988-12-19
    • MITSUBISHI ELECTRIC CORP
    • OGATA HAJIMESAITO OSAMU
    • F41G7/00B64C39/02F42B8/12F42B15/00F42B35/00
    • PURPOSE:To recover a flying body safely and prevent the leakage of secrrets and attempt to reuse the flying body by providing means to recover by the signal to detect distance in which shooting-down is not effective a flying body for test evaluation when the distance from a target to the flying body for test evaluation is over a specified distance after a fuse has generated a proximity initiation pulse or arrival initiation pulse. CONSTITUTION:A distance detection circuit 16 for distance between targets which outputs signal that detects the distance in which shooting-down is ineffective when, after an initiation pulse from the fuse has been generated, the distance between a target and a flying body for test evaluation is in excess of a specified distance is provided, and a recovery device 17 which operates when signal to detect the distance in which shooting-down is ineffective from the distance detection circuit for the distance between targets is inputted and recovers the flying body for test evaluation is provided. After a flying body N' for test evaluation which is constituted as described above is confirmed that it has traveled beyond the distance in which shooting-down in effective, the recovery device 17 operates, and it becomes possible to recover the flying body N' for test evaluation by the recovery device 17.