Magnetic Bearings for Small Satellite CMG's and Other Miniature Spacecraft Mechanisms

Award Information
Agency:
National Aeronautics and Space Administration
Amount:
$98,814.00
Program:
SBIR
Contract:
NNX11CF06P
Solitcitation Year:
2010
Solicitation Number:
N/A
Branch:
N/A
Award Year:
2011
Phase:
Phase I
Agency Tracking Number:
104403
Solicitation Topic Code:
S3.06
Small Business Information
Honeybee Robotics Ltd.
NY, New York, NY, 10001-2320
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
N
Duns:
131364820
Principal Investigator
 Kiel Davis
 Principal Investigator
 (646) 459-7809
 davis@honeybeerobotics.com
Business Contact
 Chris Chapman
Title: President
Phone: (212) 966-0661
Email: chapman@honeybeerobotics.com
Research Institution
 Stub
Abstract
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.

* information listed above is at the time of submission.

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