Application of Advanced Electromagnetic Arrays to High Efficiency, High Bandwidth, Redundant Linear Actuators

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNC05CA43C
Agency Tracking Number: 041574
Amount: $67,062.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: X6.04
Solicitation Number: N/A
Timeline
Solicitation Year: 2004
Award Year: 2005
Award Start Date (Proposal Award Date): 2005-01-19
Award End Date (Contract End Date): 2005-07-25
Small Business Information
9540 Hwy. 150, P.O. Box 250, Greenville, IN, 47124-0250
DUNS: 794955476
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Craig Rutherford
 Principal Investigator
 (865) 300-6394
 craig@katech.com
Business Contact
 David Hougland
Title: COO
Phone: (812) 923-7474
Email: david@katech.com
Research Institution
N/A
Abstract
The proposed SBIR effort will employ a systems approach to develop motor/controller/screw element systems adequate for demanding launch thrust vector control and control surface actuator applications. This approach will utilize high bandwidth, high efficiency, redundant motor systems coupled with appropriately paired motor controls. The actuator system will consist of a high efficiency permanent magnet motor with a high number of current channels for system redundancy, an H-bridge based controller with a high number of parallel current channels and sufficient current capability to enable high system response, and conventional screw-based linear actuator elements. The linear actuation elements will be designed with corrosion resistance, increased resistance to nut jamming, and inherent features preventing incorrect installation of the device. These innovations are necessary to overcome the inherent limitations of today's actuator systems, which were developed based on the limitations of traditional motors, power electronics, and available actuator hardware. Phase I of this project will focus on the design requirements, key features, and suggested solutions for thrust vector control actuator systems. The Phase II portion of the project will deliver a working prototype actuator.

* Information listed above is at the time of submission. *

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