OpportunityTitle: Thin-Wing Electromechanical Actuation (EMA) Demonstration
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.
GrantorContactEmailDescription: For Questions &amp; Assistance
GrantorContactText: Patrick Walsh &lt;br/&gt;Contract Negotiator &lt;br/&gt;Phone 937-713-9949