Advanced Materials for the Design of Lightweight JP5/JP8/DS2 Fueled Engines for UAVs

Award Information
Agency:
Department of Defense
Branch
Navy
Amount:
$68,867.00
Award Year:
2010
Program:
STTR
Phase:
Phase I
Contract:
N68335-10-C-0437
Agency Tracking Number:
N10A-001-0528
Solicitation Year:
2010
Solicitation Topic Code:
N10A-T001
Solicitation Number:
2010.A
Small Business Information
Engine Research Associates, Inc.
12108 Burning Tree Rd., Fort Wayne, IN, 46845
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
175329614
Principal Investigator:
Jeffery Erickson
Principle Investigator
(260) 338-1010
jle.erickson@verizon.net
Business Contact:
George Lewis
Vice President
(260) 485-3752
gslewis@verizon.net
Research Institution:
Purdue University
Michael R Ludwig
610 PURDUE MALL, HOVD RM 328B
WEST LAFAYETTE, IN, 47907
(765) 494-1063
Nonprofit college or university
Abstract
Develop a high power to weight, compact, heavy fuel MCC engine using advanced high strength materials. This new MCC engine design will also offer high durability and high efficiency with an extremely low acoustic and IR signature for use in future small UAVs. The overall objective of this Phase I development program is to develop a JP-5, JP-8 or DS2 MCC engine using advanced high strength to weight materials. This new design will offer a power to weight ratio between 1.1 to 1.5 HP per pound and a minimum service life over 600 hours. It will have a BSFC greater than 0.5 lb/hp-hr at all power outputs. This design will be developed for extreme operational environments including starting temperatures of 0 degrees F and above and operating temperatures from -50 degrees F to 130 degrees F. This MCC engine design can be scaled and/or stacked to cover an output range from 2 HP to 150 HP. The MCC engine is the only engine capable of full expansion which gives it an extremely quiet exhaust even without a muffler.

* information listed above is at the time of submission.

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