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.
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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 |
代理机构 |
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