Thin-Wing Electromechanical Actuation (EMA) Demonstration

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Air Force -- Research Lab

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Description

The objective of this BAA is to develop a robust, thin-wing primary flight actuator capable of achieving a high-duty cycle application (e.g. aileron) while fitting within the volume constraints mandated in future thin-wing aircraft designs. For further details, please see BAA-RQKP-2014-0011.

Who can apply

  • Unrestricted

Contact

Patrick Walsh <br/>Contract Negotiator <br/>Phone 937-713-9949
patrick.walsh.19@us.af.mil

Key dates & funding
  • PostedOct 7, 2014
  • ClosesNov 24, 2014
  • Program funding$4,000,000
  • Expected awards1
  • CFDA12.800
Categories
Science and Technology and other Research and Development

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