Robust Cryogenic Compatible Turbo-machinery and Liquid Rocket Engine coatings

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA9300-13-M-1003
Agency Tracking Number: F131-169-2045
Amount: $149,997.00
Phase: Phase I
Program: SBIR
Awards Year: 2013
Solicitation Year: 2013
Solicitation Topic Code: AF131-169
Solicitation Number: 2013.1
Small Business Information
McGaw Technology, Inc.
17439 Lake Avenue, Lakewood, OH, -
DUNS: 836682104
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Michael McGaw
 President
 (216) 521-3490
 mike@mcgawtech.com
Business Contact
 Michael McGaw
Title: President
Phone: (216) 521-3490
Email: mike@mcgawtech.com
Research Institution
N/A
Abstract
ABSTRACT: The goal of this Phase I is to demonstrate the feasibility of a ICME-based approach to the design of thermal barrier coating architectures and processes to guide the design and selection of a newly defined material/coating system, and to demonstrate this systems'ability to survive in an environment representative of a reusable oxygen-rich staged combustion engine turbine via limited, exploratory testing in test environments that mimic key characteristics of the intended operational environment. BENEFIT: The TBC modeling system and LOX-Hydrocarbon compatible TBC systems envisioned in this proposal have obvious commercial potential, especially for designers and manufacturers of reusable LOX-Hydrocarbon rocket engines. The techniques and test protocol/apparatus envisioned for the Phase II activity have clear potential for dual use in the rocket engine, aircraft engine and stationary power generation sectors.

* information listed above is at the time of submission.

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