Small UAV Hybrid Propulsion System

Award Information
Agency:
Department of Defense
Branch
n/a
Amount:
$99,880.00
Award Year:
2011
Program:
SBIR
Phase:
Phase I
Contract:
FA8650-11-M-2170
Award Id:
n/a
Agency Tracking Number:
F103-209-0692
Solicitation Year:
2010
Solicitation Topic Code:
AF103-209
Solicitation Number:
2010.3
Small Business Information
9950 Wakeman Drive, Manassas, VA, -
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
604717165
Principal Investigator:
Paul Dahlstrand
Senior Propulsion Engineer
(617) 500-4817
pdahlstrand@aurora.aero
Business Contact:
Scott Hart
Financial Analyst
(617) 500-0536
shart@aurora.aero
Research Institute:
Stub




Abstract
ABSTRACT: Aurora Flight Sciences Corporation (Aurora) proposes to conduct trade studies to determine the optimum hybrid propulsion system for an in-service UAV in the 50lb to 150lb weight range. The propulsion system will be an internal combustion (IC) engine installed in parallel with an electric motor system driving a single propeller. We are leveraging Aurora"s experience using a design tool for design space exploration and multi-objective optimization for hybrid propulsion systems in UAV applications. We will combine Aurora"s extensive UAV aircraft design experience with Mississippi State University"s automotive hybrid propulsion system design experience to provide a state-of-the-art UAV hybrid propulsion solution. BENEFIT: A hybrid propulsion system in a small UAV will allow the vehicle to operate with the benefits of both an IC engine (long endurance) and electric motor (quiet stealth) with proper design. Once a hybrid propulsion system design process is established it could be applied to virtually any existing UAV for propulsion system retrofit.

* information listed above is at the time of submission.

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