SBIR-STTR Award

Space Systems Technology Development
Award last edited on: 10/16/02

Sponsored Program
SBIR
Awarding Agency
DOD : AF
Total Award Amount
$1,479,706
Award Phase
2
Solicitation Topic Code
AF98-060
Principal Investigator
R C (Bob) Truax

Company Information

Truax Engineering Inc

1125 Adele Lane
San Marcos, CA 92069
   (760) 480-0986
   N/A
   www.rctruax.com
Location: Multiple
Congr. District: 50
County: San Diego

Phase I

Contract Number: F29601-98-C-0112
Start Date: 4/30/98    Completed: 4/12/99
Phase I year
1998
Phase I Amount
$80,000
Truax Engineering Inc. (TEI) is seeking SBIR Phase I funding to complete the initial configuration of a simple, low cost, 75,000 lb thrust, pressure fed, lattice injector, liquid rocket engine Model No. RCT-75K-097 R-1. The engine contains the following innovations aimed at lowering launch costs:A) A lattice injector design based on entirely new and different injection principle never attempted before. (Design, fabrication, and test plan details are proprietary.)B) A combustion concept that carries the possibility for suppression of combustion instability, allows reliable ignition and re-ignition, minimizes afterburning, and has the potntial for high and predictable efficiency (C*) at any scale.Project objectives:The objectives of the Phase I work are to complete the 75k engine pre-burner hydraulic proof testing, conduct water flow tests, and complete the planning for hot firing of the pre-burner at the New Mexico Tech, Energetic Materials Research Test Center (EMRTC), Rocket Test Stand (RTS), in Socorro, New Mexico.

Phase II

Contract Number: F29601-98-C-0212
Start Date: 12/1/98    Completed: 9/7/00
Phase II year
1998
Phase II Amount
$1,399,706
Truax Engineering Inc. (TEI) is seeking SBIR Phase II funding to complete the configuration of a dual use, simple, low cost, 75,000 lb thrust, pressure fed, lattice injector, liquid rocket engine Model No. RCT-75K-097 R-1 and test it at Socorro, NM. The engine contains the following innovations aimed at lowering launch costs: A) A lattice injector design based on an entirely new and different injection principle never before attempted. (Design, fabrication, and test plan details are proprietary.) B) A combustion concept that carries the possibility for suppression of combustion instability, allows reliable ignition and re-ignition, minimizes afterburning, and has the potntial for high and predictable efficiency (C*) at any scale. Project objectives: The objectives of the Phase II work are to complete the 75 K engine pre-burner hydraulic proof testing, conduct water flow tests, and complete the planning and hot firing tests of the pre-burner at the New Mexico Tech, Energetic Materials Research Test Center (EMRTC), Rocket Test Stand (RTS), in Socorro, New Mexico. Additionally, Truax Engineering is proposing to continue investigation of dual use propulsion related technologies aimed at lowering space launch costs.

Keywords:
75 K ENGINE SPACE PROPULSION TECHNOLOGIES LATTICE INJECTOR