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Magnetic Bearings for Small Satellite CMG's and Other Miniature Spacecraft Mechanisms Project
Summary
- Type of release
- a one-off release of a single dataset
- Data Licence
- Not Applicable
- Content Licence
- Creative Commons CCZero
- Verification
- automatically awarded
- Release Date
- 9 April 2015
- Modified Date
- 8 July 2015
- Publishers
- National Aeronautics and Space Administration
- Keywords
- completed, goddard-space-flight-center, project
- Identifier
- magnetic-bearings-for-small-satellite-cmgs-and-other-miniature-spacecraft-mechanisms-proje
- Landing Page
- http://techport.nasa.gov/view/9256
- Maintainers
- Gary Jahns gary.c.jahns@nasa.gov
- Language
- en-US
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Description
NASA sees an increasing role in the near future for small satellites in the 5-100 kg size range. A potentially disruptive technology, small satellites, which are low cost and can be delivered in months, are being eyed as platforms for rapid demonstration of new technologies and even important science missions. From NASA's recently launched PharmaSat sub-10 kg free-flying nanosatellite, which has just successfully completed an experiment that could help scientists better understand how effectively drugs work in space, to potential future missions like CRESPO, a ~100 kg microsatellite that will use a hyperspectral imager to monitor the condition of more than 50% of the Earth's coral reefs over a 2-year period, NASA is counting on these small satellites to deliver. A miniature PMB technology is widely applicable to small mechanisms and will allow for a greater technological payoff with the next generation of small satellite missions. Honeybee Robotics is developing a small, modular control moment gyroscope (CMG) technology for use on small satellites. The life limiting and power driving aspect of this technology as with any CMG or reaction wheel (RW), are the rotor bearings which operate at 12,000 rpm. Honeybee Robotics proposes to develop a miniature passive magnetic bearing (PMB) for small satellite ACS components such as CMGs and RWs. This cross-cutting technology can also be applied to any small mechanism that might benefit from low parasitic torque, low induced vibration (IV), and long life. PMB technology for small satellites will allow for a step increase in life for their ACS subsystems. Enabling a small satellite mission lifetime of 15+ years rather than 1-3 years is a game-changing development that will alter the way mission planners think about small satellite capabilities. Prototype units will be integrated with our Tiny Operationally Responsive CMG (TORC) technology to demonstrate the relative merits compared to traditional ball bearings.
General Information
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This data is described at
http://catalog.data.gov/dataset/magnetic-bearings-for-small-satellite-cmgs-and-other-miniature-spacecraft-mechanisms-proje Do you think this data is incorrect? Let us know
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This data is published by
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Legal Information
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The rights statement is at
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Outside the US, this data is available under
Creative Commons CCZero Do you think this data is incorrect? Let us know
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There are
yes, and the rights are all held by the same person or organisation Do you think this data is incorrect? Let us know
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The content is available under
Creative Commons CCZero Do you think this data is incorrect? Let us know
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its data licence Do you think this data is incorrect? Let us know
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This data contains
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Practical Information
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The data appears in this collection
http://catalog.data.gov/organization/nasa-gov Do you think this data is incorrect? Let us know
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The accuracy or relevance of this data will
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The data is
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Technical Information
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This data is published at
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Find out how to suggest improvements to publication at
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