SBIR/STTR Research Award

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

Award identifier 69a711dcf1b09f4ce1f2e0c6db62e502916560ddf44c8a5d2569e757b52e38b1Awarding agency National Aeronautics and Space Administration

Award amount

$98,814

Program and phase

SBIR · Phase I

Award year

2011

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Honeybee Robotics, Ltd.
Proposal award date
2011-02-18
Contract end date
2011-09-29
UEI
F7UHKQTEYHW8
Solicitation number
Not reported
Topic code
S3.06

Research 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.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

116 SBIR/STTR records share this UEI (1991–2017). Reported award amounts total $36,289,766. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense, National Science Foundation

Agency intelligence

National Aeronautics and Space Administration

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