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.
申请公布号
WO2007001426(A2)
申请公布日期
2007.01.04
申请号
WO2005US37835
申请日期
2005.10.21
申请人
HONEYWELL INTERNATIONAL INC.;JACOBS, JACK, H.;PECK, MASON, A.