DocumentCode
1240274
Title
HTS bearings for space applications: reaction wheel with low power consumption for mini-satellites
Author
Ma, Ki B. ; Zhang, Yong ; Postrekhin, Yevgeniy ; Chu, Wei-Kan
Author_Institution
Texas Center for Supercond., Univ. of Houston, TX, USA
Volume
13
Issue
2
fYear
2003
fDate
6/1/2003 12:00:00 AM
Firstpage
2275
Lastpage
2278
Abstract
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 15000 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.
Keywords
aerospace instrumentation; artificial satellites; attitude control; high-temperature superconductors; magnetic bearings; angular momentum; attitude control; friction coefficient; high temperature superconductor magnet bearing; mini-satellite; power consumption; space vehicle; spin down test; stainless steel reaction wheel; Energy consumption; Friction; Hardware; High temperature superconductors; Performance evaluation; Power measurement; Prototypes; Steel; Testing; Wheels;
fLanguage
English
Journal_Title
Applied Superconductivity, IEEE Transactions on
Publisher
ieee
ISSN
1051-8223
Type
jour
DOI
10.1109/TASC.2003.813064
Filename
1212074
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