C-CCarbon-Carbon
- Matrix
- Carbon
- Best at
- Highest temperature, up to 3000°C
- Typical parts
- Nozzle throats
- Leading edges
- Furnace hardware
Built for
extremes
Carbon-carbon, C-SiC and UHTC composites, and the Film Boiling CVI systems that make them. Designed and built in Bengaluru.
Carbon-Carbon
Carbon fibre in a carbon matrix. Rated up to 3000°C, dimensionally stable and resistant to erosion and wear. The material for nozzle throats, leading edges and furnace hardware.
3000°CThermal rating
Erosion resistantTribological
StableDimensionally
C-SiC
A silicon carbide matrix adds high oxidation resistance and wear tolerance. Built for hot structures and friction parts, including carbon-ceramic brake discs.
Request a datasheet
Structural composites
Carbon fibre reinforced polymer parts that are light, strong and stiff. For aerospace structures, UAVs and industrial components.
Discuss your partWhich material fits your part?
A quick guide to our three composite families. Hover over a card to see where each one shines.
C-CC-SiCCarbon-Silicon Carbide
- Matrix
- Silicon carbide
- Best at
- Oxidation resistance and wear tolerance
- Typical parts
- Hot structures
- Friction parts
- Brake discs
C-FRPStructural composites
- Matrix
- Polymer
- Best at
- Light, strong and stiff
- Typical parts
- Aerospace structures
- UAVs
- Industrial components
Film Boiling CVI
Our proprietary densification process. A carbon precursor boils around a heated preform, filling the pores faster and more uniformly than conventional isothermal CVI.
FasterProcess cycles
UniformDeposition
LowerPorosity
We also build isothermal CVI and graphitisation reactors up to 3000°C, and FEA-validated composite tooling molds.
Enquire about systemsWhere our materials go to work
Six industries that depend on materials that survive extreme heat, wear and speed.
Launch vehicles
Thermal protection systems, hot structures and reentry components.
- Thermal protection
- Hot structures
- Reentry
Defense
Hypersonic nose cones and leading edges that endure high-Mach flight.
- Hypersonic
- Leading edges
- High Mach
Satellites
Dimensionally stable structures for precision optics in space.
- Dimensional stability
- Precision optics
- Space environment
Propulsion
Nozzle divergents and throat inserts that resist erosion at high temperature.
- Nozzle divergents
- Throat inserts
- Erosion resistant
Semiconductor
Crucibles, heaters and support structures for pure, precise fabs.
- Crucibles
- Heaters
- Support structures
Automotive
Carbon-ceramic brake discs for performance and reliability.
- Carbon-ceramic discs
- Performance
- Reliability
Concept to flight, one roof
Design, simulation, tooling, process and qualification run in parallel, with no hand-offs between suppliers.
Design
Parts engineered for the thermal and structural load they will see.
Simulation
CFD, FEA and digital twins that cut trial and error.
Tooling
Molds validated by FEA before material is committed.
Process
FB-CVI and isothermal CVI, graphitisation to 3000°C.
Qualification
Testing by the team that built the part.
High-temperature coatings
Siliconization, carbide-forming barriers and ultra-high-temperature ceramics (UHTCs) extend composites beyond 2000°C and protect them from oxidation.
Founder photo
20+Years in space and defense programs
A note from our founder
I have spent more than twenty years on space and defense programs. I started Mysitech to push high-temperature composites and the processes behind them further, and to make India a source of these technologies.
We invest in R&D partnerships, academic collaboration and intellectual property, so that our process equipment, composite systems and simulation-based design keep moving forward.
Dr. Jhon PaulFounder · Innovation. Integration. Impact.
- R&D partnerships
- Academic collaboration
- IP-driven innovation
Have a part in mind?
Tell us the temperature and the load.
Questions
What are carbon-carbon (C-C) composites?
Carbon fibres in a carbon matrix. They keep their strength at temperatures where metals fail, with ratings up to 3000°C, and are used in rocket nozzles, hypersonic leading edges, brakes and furnace hardware.
What is Film Boiling CVI?
A densification process in which a carbon precursor boils around a heated preform, filling the pores of a fibre structure faster and more uniformly than conventional isothermal CVI.
What is the difference between C-C and C-SiC?
C-C offers the highest temperature capability. C-SiC adds a silicon carbide matrix for better oxidation resistance and wear tolerance in hot structures and friction parts.
Which industries does Mysitech serve?
Launch vehicles, defense, satellites, propulsion, semiconductor and industrial furnaces, and automotive brake systems.
Tell us the temperature and the load
Share your application, environment and timeline. An engineer will reply.
Emailtechnical@mysitech.comPhone+91-9633889898
Office#37, 9th Cross, Brundavana Nagar, Ward No. 40, Karihobanahalli, Nagasandra Post, Bengaluru, Karnataka 560073, India