发明名称 |
Semi-active laser seeker gyroscope |
摘要 |
A gyro in which an elastomeric material is used as a spherical bearing surface in an air bearing type gyro to sustain 12,500 g set back acceleration level during gun launch and have the capability of surviving the launch phase in a non-functioning mode and then being operative in post-launch lower-g environments as a stabilized/torquing seeker capable of tracking laser illuminated moving target so as to enable the gyro to be used for guided projectile systems.
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申请公布号 |
US4246801(A) |
申请公布日期 |
1981.01.27 |
申请号 |
US19790008464 |
申请日期 |
1979.02.01 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY |
发明人 |
RODGERS, AUBREY;ROBERTSON, WILLIAM G. |
分类号 |
F41G7/22;G01C19/20;G01C19/26;(IPC1-7):G01C19/12 |
主分类号 |
F41G7/22 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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