HTS bearings for space applications: Reaction wheel with low power consumption for mini-satellites

被引:16
作者
Ma, KB [1 ]
Zhang, Y [1 ]
Postrekhin, Y [1 ]
Chu, WK [1 ]
机构
[1] Univ Houston, Texas Ctr Superconduct, Houston, TX 77204 USA
关键词
attitude control; low power consumption; reaction wheel; superconductor magnet bearings;
D O I
10.1109/TASC.2003.813064
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Superconducting bearings have very low coefficients of friction. It is promising to exploit this feature of HTS bearings in the construction of reaction wheel systems that consume meager power. Reaction Wheel systems that consume little power are particularly suitable for use on mini-satellites where both energy and power are, scarce resources. Thus, these mini-satellites can still have attitude control capabilities without prohibitive requirements for total volume and weight of hardware, and power consumption. Here, we Will present the design and discuss the performance of a prototype with a 1.9 kg stainless steel wheel of diameter 82.5 mm, and height 75 mm, which can store 3.5 J-sec of angular momentum when it rotates at-an angular speed, of 15,000 RPM. We have performed spin down tests from 7000 RPM down and measured the input power required, to sustain rotational speed under a vacuum of 0.01 torr. Implications of the results are discussed.
引用
收藏
页码:2275 / 2278
页数:4
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