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SiC-SiC and C-SiC Honeycomb for Advanced Flight Structures
Completed
TRL 4 (started at 3, targeting 4)
Description
The proposed project builds upon the work done in Phase I with the development of a C-SiC CMC honeycomb material that was successfully tested for mechanical properties at both ambient and high temperature. The further study expands to include the development of an SiC-SiC honeycomb using the proven infiltration process of the Phase I project. In the proposed project, an SiC prepreg will be engineered that can be formed into a honeycomb and then infiltrated with SiC to form a ceramic SiC-SiC honeycomb. The honeycomb will then be tested mechanically at ambient temperature and high temperature. This testing will include cycling the material to determine property falloff. C-SiC and SiC SiC will be compared in this study. The thermal characteristics, such as conductivity and emissivity, will also be tested. The integration of such a material into hypersonic and other structures is a key area of the research; therefore a bonding study is included in the current proposal. Several bonding technologies and processes will be investigated and tested mechanically as well as cycled to determine durability. The goal of the study is to provide a sandwich level technology that can be integrated into hypersonic vehicle structures and acreage.
Benefits
The material could be useful in any application where the weight of SiC is an issue. For example, mirror structures made from SiC could be significantly lightweighted using SiC-SiC honeycomb.
The primary commercial application for such materials is in hypersonic flight vehicles. A durable, lightweight material that can be integrated into acreage and structures is a key enabler of designing and building a multi-cycle hypersonic vehicle. These materials could also be considered for integration into a variety of other thermal protection systems.
Details
| Technology area | Thermal Management Systems > Thermal Control Components and Systems > Insulation and Interfaces |
| Program | Small Business Innovation Research/Small Business Tech Transfer (SBIR/STTR) |
| Lead organization | Ultracor, Livermore, CA |
| Start date | 2011-06-01 |
| End date | 2013-11-30 |
Project contacts
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How to get involved
This is early/mid-stage (TRL 4) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.
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