发明名称 Rocket elevation angle measuring device - has pendulum positioning itself into firing direction by take-off acceleration
摘要 <p>The measuring device determines and stores the angle of elevation on a launched rocket for evaluation and activation of certain switching and/or control functions. The rocket has a measuring system which determines the angle of elevation and stores the measured value for subsequent evaluation to take place after the firing. The measuring system consists of a housing contg. a potentiometer. The set spindle of the potentiometer carries a toothed wheel in mesh with an intermediary wheel only during the acceleration phase. The intermediary wheel is fitted on a shaft seated on a lateral bearing on the side which carries the intermediate wheel. The other side of the shaft carries out limited swinging movements around the bearing.</p>
申请公布号 DE2557317(A1) 申请公布日期 1977.06.30
申请号 DE19752557317 申请日期 1975.12.19
申请人 VEREINIGTE FLUGTECHNISCHE WERKE-FOKKER GMBH 发明人 SEEGER,HANS-JOCHEN,DIPL.-ING.
分类号 F41G3/12;F41G7/00;(IPC1-7):41G7/14 主分类号 F41G3/12
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