Lightweight Ultrahigh Temperature CMC-Lined C/C Combustion Chambers

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNC06CA82C
Agency Tracking Number: 054694
Amount: $70,000.00
Phase: Phase I
Program: SBIR
Awards Year: 2006
Solicitation Year: 2005
Solicitation Topic Code: X2.01
Solicitation Number: N/A
Small Business Information
Ultramet
12173 Montague St, Pacoima, CA, 91331-2210
DUNS: 052405867
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Gautham Ramachandran
 Principal Investigator
 (818) 899-0236
 gautham.ramachandran@ultramet.com
Business Contact
 Craig Ward
Title: Engineering Administrative Mgr
Phone: (818) 899-0236
Email: craig.ward@ultramet.com
Research Institution
N/A
Abstract
NASA and DoD are seeking economical and high-performance bipropellant thrusters for various applications. These goals cannot be achieved using the silicided C103 chambers in current use. Ultramet has developed and successfully demonstrated carbon fiber-reinforced zirconium carbide (C/ZrC) and carbon fiber-reinforced zirconium-silicon carbide (C/Zr-Si-C) ceramic matrix composites (CMCs) for use in liquid propellant applications up to 4200oF. Although the density of these CMCs is less than that of C103, further reducing overall weight is desired with a target goal of 2.6 g/cm3. Carbon/carbon (C/C) is widely used because of its light weight and high specific strength at elevated temperatures. However, adequate long-term protection of C/C is the limiting factor for its use in liquid propellant propulsion components. Ultramet will combine the light weight of C/C and the ultrahigh temperature oxidation resistance of C/Zr-Si-C CMCs in a unique laminate composite. This system will possess an overall density that is similar to C/SiC while increasing the operating temperature to 4000oF in liquid propulsion applications. Net-shape fabrication of CMC-lined C/C combustion chambers will be accomplished by adapting an innovative variant of Ultramet's melt infiltration technology.

* information listed above is at the time of submission.

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