SBIR/STTR Research Award
Carbon-Carbon High Melt Coating for Nozzle and Nozzle Extensions
Award amount
$99,366Program and phase
SBIR · Phase IAward year
2010Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- Carbon Carbon Advanced Technologies, Inc.
- Proposal award date
- 2010-01-29
- Contract end date
- 2010-07-29
- UEI
- N3NULR7A1A88
- Solicitation number
- Not reported
- Topic code
- X10.01
Research abstract
C-CAT, which has proven carbon-carbon fabrication capabilities, will investigate use of ACC-6 High Melt oxidation protective system on carbon-carbon for use on the Cryogenic and Non-Toxic Storable Propellant Space Engine nozzle and nozzle extensions.
ACC-6 High Melt is a carbon-carbon coating application that embeds HfC,ZrB2 in the outer layers. This material system has been tested in Arc Jet environment at over 3000 degrees F, for more than 24 minutes with little to no erosion. ACC-6 High Melt has shown to be the best performing high temperature material system, and still retains the ease of manufacturing associated with carbon-carbon.
ACC-6 High Melt has been manufactured in small scale leading edge experiments, but has yet to be demonstrated in large components. Manufacturability of large scale components remains as the main question to be answered for this material system. For Phase I, C-CAT proposes to build subsections of a nozzle extension representing the attach flange and the exit diameter of approximately 40" diameter. Success will be achieved by manufacturing the aforementioned subsection using ACC-6 High Melt with no voids or spalling of coating. This successful demonstration will provide the path for scale-up to a full size prototype nozzle extension for Phase II.
Technology keywords
Not reported
Other awards by this recipient
Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.
- Extreme Temperature Structures
- Design and Manufacture of a Prototype Hypersonic Glide Vehicle Target Using C-CAT ACC Materials
- Accelerated Processing with Geometry-Specific Pyrolysis Heating Profiles for Production of C-C Hot Structures
- ACC Enhanced with Ceramic Matrix via Reactive Melt Infiltration for Scramjet Duct Applications
- Extreme Temperature Stitched Structures
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Reliable Actuator for Cryo Propellant Fluid Control
- Thin Aerogel as a Spacer in Multi-Layer Insulation for Cryogenic Space Applications
- A Novel Flow Measurement System for Cryogenic Two-Phase Flow
- Reliable Actuator for Cryo Propellant Fluid Control
- Thin Aerogel as a Spacer in Multi-Layer Insulation for Cryogenic Space Applications