发明名称 Aeroballistic diagnostic system
摘要 A system which is packaged within a projectile fuze body and obtains data relative to the projectile during a launch. Sensors are provided which obtain in-bore data as well as in-flight data. The in-bore data is recorded at a fast rate during in-bore travel of the projectile and is read out, continuously, at a slower rate during in-flight travel. Both in-bore data and in-flight data are encoded and transmitted to a ground station for analysis.
申请公布号 US6349652(B1) 申请公布日期 2002.02.26
申请号 US20010770780 申请日期 2001.01.29
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY 发明人 HEPNER DAVID J.;HOLLIS MICHAEL S. L.;MULLER PETER C.;HARKINS THOMAS E.;BORGEN GARY;D'AMICO WILLIAM P.;DAVIS BRADFORD S.;BURKE LAWRENCE W.
分类号 F42B15/01;F42B30/00;F42C19/00;(IPC1-7):F42B10/00;F42C17/00 主分类号 F42B15/01
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