Thin-Wing Electromechanical Actuation (EMA) Demonstration
The summary for the Thin-Wing Electromechanical Actuation (EMA) Demonstration grant is detailed below.
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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-2014-0011.
Federal Grant Title: | Thin-Wing Electromechanical Actuation (EMA) Demonstration |
Federal Agency Name: | Air Force Research Lab |
Grant Categories: | Science and Technology |
Type of Opportunity: | Discretionary |
Funding Opportunity Number: | RQKP-2014-0011 |
Type of Funding: | Cooperative Agreement, Grant, Procurement Contract |
CFDA Numbers: | 12.800 |
CFDA Descriptions: | Air Force Defense Research Sciences Program |
Current Application Deadline: | Nov 10, 2014 |
Original Application Deadline: | Nov 10, 2014 |
Posted Date: | October 7th, 2014 |
Creation Date: | Oct 7, 2014 |
Archive Date: | Dec 10, 2014 |
Total Program Funding: | $4,000,000 |
Maximum Federal Grant Award: | none |
Minimum Federal Grant Award: | none |
Expected Number of Awards: | 1 |
Cost Sharing or Matching: | No |
- Applicants Eligible for this Grant
- Unrestricted (i.e., open to any type of entity above), subject to any clarification in text field entitled "Additional Information on Eligibility"
- Grant Announcement Contact
- Patrick Walsh
Contract Negotiator
Phone 937-713-9949
For Questions & Assistance
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