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Thin-Wing Electromechanical Actuation (EMA) Demonstration
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-2014-001
1.
aileron) while fitting within the volume constraints mandated in future thin-wing aircraft designs.
For further details, please see BAA-RQKP-2014-001
1.
Agency: Department of Defense
Office: Air Force -- Research Lab
Estimated Funding: $4,000,000
Office: Air Force -- Research Lab
Estimated Funding: $4,000,000
Obtain Full Opportunity Text:
Not Available
Additional Information of Eligibility:
Not Available
Full Opportunity Web Address:
Contact:
Patrick WalshContract NegotiatorPhone 937-713-9949
Agency Email Description:
For Questions & Assistance
Agency Email:
patrick.walsh.19@us.af.mil
Date Posted:
2014-10-07
Application Due Date:
2014-11-24
Archive Date:
2014-12-10
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