USA flag logo/image

An Official Website of the United States Government

Company Information:

Name: Electronic Concepts &
Address: 4750 West Bancroft St.
Toledo, OH 43606
Located in HUBZone: No
Woman-Owned: No
Minority-Owned: No
URL: N/A
Phone: N/A

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $226,748.00 3
SBIR Phase II $631,393.00 3

Award List:

ULTRA LOW COST ENGINE CONTROL SYSTEM

Award Year / Program / Phase: 1991 / SBIR / Phase I
Agency / Branch: DOD / DARPA
Principal Investigator:
Award Amount: $59,475.00

ULTRA LOW COST ENGINE CONTROL SYSTEM

Award Year / Program / Phase: 1993 / SBIR / Phase II
Agency / Branch: DOD / DARPA
Principal Investigator:
Award Amount: $236,888.00
Abstract:
Present turbojet engine control systems, which are comprised of: controller, fuel metering device, sensors, connectors, and harnesses are the single most expensive subsystem on expendable turbojet engines. the size and cost of expendable turbojet engines has steadily decreased. however, the engine… More

Universal Propulsion System Controller

Award Year / Program / Phase: 1994 / SBIR / Phase I
Agency / Branch: DOD / ARMY
Principal Investigator: William Swonger
Award Amount: $69,814.00

Universal Tactical Missile Propulsion System Simulator

Award Year / Program / Phase: 1995 / SBIR / Phase I
Agency / Branch: DOD / DARPA
Principal Investigator: Karl Swonger
Award Amount: $97,459.00
Abstract:
The next generation of tactical missiles will use several types of non-traditional propulsion systems, each of which requires a control system. A method is required to economically and thoroughly evaluate and analyze the propulsion control system without risking expernsive, one-of-a-kind, prototype… More

Universal Propulsion System Controller

Award Year / Program / Phase: 1995 / SBIR / Phase II
Agency / Branch: DOD / ARMY
Principal Investigator: William Swonger
Award Amount: $241,389.00
Abstract:
Presently, missile propulsion systems use a custom designed, application specific, control system to govern thrust variation. A custom designed and application specific missilized component is costly. Therefore, ECE proposes to apply a single, universal, low cost thrust controller design to many… More

Universal Tactical Missile Propulsion System Simulator

Award Year / Program / Phase: 1998 / SBIR / Phase II
Agency / Branch: DOD / DARPA
Principal Investigator: Karl Swonger
Award Amount: $153,116.00
Abstract:
The next generation of tactical missiles will use several types of non-traditional propulsion systems, each of which requires a control system. A method is required to economically and thoroughly evaluate and analyze the propulsion control system without risking expernsive, one-of-a-kind, prototype… More