发明名称 |
Momentum tube for distributed actuation |
摘要 |
An spacecraft control system is provided that includes a tube and a plurality of microwheels. The plurality of microwheels is disposed within the tube. Each microwheel has a first stator wafer, a second stator wafer, and a rotor wafer disposed therebetween. The first and second stator wafers are configured to spin the rotor wafer.
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申请公布号 |
US7367529(B2) |
申请公布日期 |
2008.05.06 |
申请号 |
US20040971270 |
申请日期 |
2004.10.22 |
申请人 |
HONEYWELL INTERNATIONAL, INC. |
发明人 |
JACOBS JACK H.;PECK MASON A. |
分类号 |
B64G1/28 |
主分类号 |
B64G1/28 |
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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