SBIR/STTR Research Award
Interface Coatings for Carbon and Silicon Carbide Fibers in Silicon Carbide Matrixes
Award amount
$69,880Program and phase
SBIR · Phase IAward year
2004Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- Synterials, Inc
- Proposal award date
- 2004-01-16
- Contract end date
- 2004-07-19
- UEI
- Not reported
- Solicitation number
- Not reported
- Topic code
- A4.03
Research abstract
Interface coatings for fiber-reinforced composites are an enabling
technology for high temperature ceramic matrix composites. Because of
their availability and relative cost, graphite fibers are preferred for
many structural composite of interest for space propulsion applications.
However, high temperature stable silicon carbide fibers are also of
interest, even though they are higher cost. Recent work at Synterials,
has suggested that a thin layer of carbon at the surface of the fiber is
key to preventing corrosion of the fiber and subsequent fiber strength
reduction on graphite fibers. The proposed work will evaluate three
interface coatings one three graphite fibers and one silicon carbide
fiber. The coating are: B4C, Si-doped BN/Si3N4 and HfC. The coatings
will be evaluated by preparing mini-composites via a polymer plus CVI
processing route.
Technology keywords
Not reported
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Actively Cooled Ceramic Composite Nozzle Material
- Actively Cooled Ceramic Composite Nozzle Material
- Oxidation Resistant CMC Materials Technology for Lightweight and Environmentally Durable Propulsion Components