Aircraft Drag Reduction Program

 

The objective of the Aircraft Drag Reduction Program will be to mature and transition technologies to reduce the fuel burn of legacy and future fleet aircraft by employing engineered surfaces, materials, and coatings (ESMC). Aircraft drag reduction by means of ESMC may address any element of aircraft drag. This Research and Development (R&D) may include, aircraft drag reduction technologies, especially turbulent boundary layer skin friction drag reduction; evaluating the performance (drag reduction) of the technologies – tests ranging from laboratory testing of ESMC coupons, to wind tunnel testing (small- to large-scale), to flight testing of ESMC technologies; and maturing and transitioning technologies to aircraft, to include qualification testing of new coatings, materials, or surfaces.

General information about this opportunity
Last Known Status
Deleted 11/11/2014 (Archived.)
Program Number
BAA-RQKPC-2014-0004
Federal Agency/Office
Agency: Department of Defense
Office: Department of the Air Force, Research Lab
Type(s) of Assistance Offered
Cooperative Agreement, Procurement Contract
Number of Awards Available
1
What is the process for applying and being award this assistance?
Deadlines
10/27/2014
Other Assistance Considerations
Formula and Matching Requirements
This program does not have cost sharing or matching requirements.
Who do I contact about this opportunity?
Headquarters Office
Steven Brumfield
Contracting Officer
Phone 937-713-9934
E-mail Address
steven.brumfield.1@us.af.mil
Financial Information
Obligations
$8,750,000.00

 


Related Federal Grants


Federal Grants Resources