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Company Information:

Company Name:
Technical Directions Inc.
Address:
1210 Oakbrook Drive
Ortonville, MI
Phone:
(248) 625-2990
URL:
EIN:
382354963
DUNS:
121523815
Number of Employees:
3
Woman-Owned?:
No
Minority-Owned?:
No
HUBZone-Owned?:
No

Commercialization:

Has been acquired/merged with?:
N/A
Has had Spin-off?:
N/A
Has Had IPO?:
N/A
Year of IPO:
N/A
Has Patents?:
N/A
Number of Patents:
N/A
Total Sales to Date $:
$ 0.00
Total Investment to Date $
$ 0.00
POC Title:
N/A
POC Name:
N/A
POC Phone:
N/A
POC Email:
N/A
Narrative:
N/A

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $296,122.00 4
SBIR Phase II $4,841,387.00 7

Award List:

CERAMIC COMPONENT FEASIBILITY DEMONSTRATION IN A SMALL TURBOJET ENGINE

Award Year / Program / Phase:
1989 / SBIR / Phase I
Award Amount:
$49,751.00
Agency / Branch:
DOD / ARMY
Principal Investigator:
Vern E Brooks
Abstract:
N/a

CERAMIC COMPONENT FEASIBILITY DEMONSTRATION IN A SMALL TURBOJET ENGINE

Award Year / Program / Phase:
1991 / SBIR / Phase II
Award Amount:
$478,973.00
Agency / Branch:
DOD / ARMY
Principal Investigator:
Vern E Brooks
Abstract:
An operational demonstration of the technical feasibility of a high temperature small turbojet engine is provided by this program. this demonstration confirms that a ceramic radial turbine wheel can withstand the short duration high temperature exposure required of a small tactical missile engine.… More

FEASIBILITY DEMONSTRATION OF LOW COST INTEGRAL STARTER/GENERATOR FOR SMALL TURBOJET

Award Year / Program / Phase:
1991 / SBIR / Phase I
Award Amount:
$49,925.00
Agency / Branch:
DOD / ARMY
Principal Investigator:
Vern E Brooks , Principal Investigator
Abstract:
N/a

FEASIBILITY DEMONSTRATION OF LOW COST INTEGRAL STARTER/GENERATOR FOR SMALL TURBOJET

Award Year / Program / Phase:
1992 / SBIR / Phase II
Award Amount:
$485,344.00
Agency / Branch:
DOD / ARMY
Principal Investigator:
Vern E Brooks , Principal Investigator
Abstract:
An operational demonstration of the technical feasibility of a low cost integral starter/generator for small turbojet engines is provided by this program. a unique dual purpose starter/generator control concept is employed which uses only one-third of the power switching devices of conventional… More

Low-Cost Propulsion System for Smart Munitions

Award Year / Program / Phase:
1999 / SBIR / Phase I
Award Amount:
$98,846.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Vern Brooks
Abstract:
N/a

Low-Cost Propulsion System for Smart Munitions

Award Year / Program / Phase:
2000 / SBIR / Phase II
Award Amount:
$738,693.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Vern E. Brooks
Abstract:
N/a

Aeropropulsion and Power Technology

Award Year / Program / Phase:
2005 / SBIR / Phase I
Award Amount:
$97,600.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Vern E. Brooks, President
Abstract:
Small low-cost propulsion systems are required for a variety of new unmanned air vehicle applications. Turbojet engine-generator systems are considered desirable for these small aircraft applications where compact size and low-cost are critical parameters. Technical Directions Inc. has developed a… More

Aeropropulsion and Power Technology

Award Year / Program / Phase:
2006 / SBIR / Phase II
Award Amount:
$736,487.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Joseph J. Kovasity, SENIOR PROJECT ENGINEER
Abstract:
Small low-cost propulsion systems are required for a variety of new unmanned air vehicle applications. Turbojet engine-generator systems are considered desirable for these small aircraft applications where compact size and low-cost are critical parameters. Technical Directions Inc. has developed a… More

Aeropropulsion and Power Technology

Award Year / Program / Phase:
2010 / SBIR / Phase II
Award Amount:
$748,236.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Joseph J. Kovasity, Chief Engineer
Abstract:
Technical Directions Inc. (TDI) has demonstrated a state-of-the-art method of designing small turbine engine compressor and turbine components for very small turbojet engine-generator applications. This program will transfer this technology to compact Auxiliary Power Units (APUs) for airborne and… More

Aeropropulsion and Power Technology

Award Year / Program / Phase:
2010 / SBIR / Phase II
Award Amount:
$928,235.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Joseph J. Kovasity, Chief Engineer – (248) 625-2990
Abstract:
Technical Directions Inc. (TDI) has demonstrated a state-of-the-art method of designing small turbine engine compressor and turbine components for very small turbojet engine-generator applications. This program will transfer this technology to compact Auxiliary Power Units (APUs) for airborne and… More

PROPULSION SYSTEM FOR POWERED GRAVITY WEAPON

Award Year / Program / Phase:
2013 / SBIR / Phase II
Award Amount:
$725,419.00
Agency:
DOD
Principal Investigator:
Joseph J. Kovasity, VICE PRESIDENT – (248) 625-2990
Abstract:
ABSTRACT: Technical Directions Inc. (TDI) has developed a family of low cost propulsion systems for small air vehicles that will provide all necessary propulsion functions for sustained flight. A turbine-based engine-generator is utilized to provide the vehicle propulsion and all necessary… More