USA flag logo/image

An Official Website of the United States Government

Company Information:

Name: AJT and Associates, Inc
Address: 8910 Astronaut Blvd
Cape Canaveral, FL 32920
Located in HUBZone: No
Woman-Owned: No
Minority-Owned: Yes
URL: N/A
Phone: (321) 783-7989

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $139,985.00 3
SBIR Phase II $613,900.00 1

Award List:

Auto-Coupler System for Engine Test Stands

Award Year / Program / Phase: 1999 / SBIR / Phase I
Agency: NASA
Principal Investigator: Tracey Post, Principcal Investigator
Award Amount: $69,985.00

Low Cost Engine Test Stand for 500 lb Thrust Class Engines

Award Year / Program / Phase: 2001 / SBIR / Phase I
Agency: NASA
Principal Investigator: Dr. 1. Wegerif, Manager, Mechanical Systems
Award Amount: $70,000.00
Abstract:
AJT proposes to develop a low-cost, engine test-stand system for small (500 pound) thrust engines using gaseous, liquid or cryogenic propellants. This test stand would incorporate automated propellant transfer and automated propellant line purge systems. The engines would be configured to a standard… More

Low Cost Engine Test Stand for 500 lb Thrust Class Engines

Award Year / Program / Phase: 2002 / SBIR / Phase I
Agency: NASA
Principal Investigator: Dr. Wegerif, Manager, Mechanical Systems
Award Amount: $0.00
Abstract:
AJT proposes to develop a low-cost, engine test-stand system for small (500 pound) thrust engines using gaseous, liquid or cryogenic propellants. This test stand would incorporate automated propellant transfer and automated propellant line purge systems. The engines would be configured to a standard… More

Low Cost Engine Test Stand for 500 lb Thrust Class Engines

Award Year / Program / Phase: 2002 / SBIR / Phase II
Agency: NASA
Principal Investigator: Dr. Wegerif, Manager, Mechanical Systems
Award Amount: $613,900.00
Abstract:
AJT proposes to develop a low-cost, engine test-stand system for small (500 pound) thrust engines using gaseous, liquid or cryogenic propellants. This test stand would incorporate automated propellant transfer and automated propellant line purge systems. The engines would be configured to a standard… More