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C/C Composite 3D

Grade

also Carbon-Carbon

3D = 3D woven / orthogonal preform C/C

Choose when through-thickness strength and delamination resistance are critical (nozzles, throats, brake discs, re-entry structures).

High cost $$$$

Values for the 3D condition

Other C/C Composite tempers and conditions

C/C Composite is listed in 3 conditions; see the grade overview at C/C Composite.

Compare all 3 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
needled carbon-felt preform, CVI/impregnation densified
Lowest-cost route for large furnace hardware (crucibles, heaters, guide cylinders) where stiffness matters less than thermal stability.—90——20 W/m·K
mesophase-pitch fiber, high thermal conductivity C/C
Pick for thermal-management / heat-spreader and high-energy brake duty where in-plane conductivity above 200 W/m·K is required.—1500.1545 HV300 W/m·K
3DThis page
3D woven / orthogonal preform C/C
Choose when through-thickness strength and delamination resistance are critical (nozzles, throats, brake discs, re-entry structures).—180——50 W/m·K

What is C/C Composite 3D?

C/C Composite 3D is C/C Composite in the 3D grade — choose when through-thickness strength and delamination resistance are critical (nozzles, throats, brake discs, re-entry structures). C/C Composite 3D has a tensile strength of 180 MPa (26.1 ksi), stronger than 57% of ceramic grades. Elongation at break is 0.4% and the elastic modulus is 70 GPa (10.2 Msi). C/C Composite 3D has a density of 1.85 g/cm³ (0.0668 lb/in³), lighter than 88% of ceramic grades. It melts at 3,650°C (6,602 °F).

Advantages

  • High service temperature — 2,500°C (4,532 °F), better than 98% of ceramic grades
  • Ductile — tolerates forming and impact — 0.4%, better than 96% of ceramic grades
  • Lightweight — 1.85 g/cm³ (0.0668 lb/in³), better than 88% of ceramic grades
  • Easy to machine — 25/100, better than 84% of ceramic grades
  • Tough — resists crack growth — 8 MPa·√m (7.28 ksi·√in), better than 77% of ceramic grades

Limitations

  • Hard to polish — 20/100, worse than 99% of ceramic grades
  • High embodied carbon — 55 kg CO₂/kg, worse than 97% of ceramic grades
  • Low stiffness — 70 GPa (10.2 Msi), worse than 79% of ceramic grades

C/C Composite 3D properties

Typical room-temperature values for C/C Composite 3D; 11 are specific to this condition. Other listed values are C/C Composite reference data and may not represent this condition. Bars are the position among ceramic grades.

Physical3

C/C Composite 3D has a density of 1.85 g/cm³ (0.0668 lb/in³), lighter than 88% of ceramic grades. It melts at 3,650°C (6,602 °F).

Density1.85 g/cm³0.07 lb/in³
Melting Point (Solidus)3,650°C6,602 °F
Porosity7%

Mechanical9

C/C Composite 3D has a tensile strength of 180 MPa (26.1 ksi), stronger than 57% of ceramic grades. Elongation at break is 0.4% and the elastic modulus is 70 GPa (10.2 Msi).

Elastic (Young's) Modulus70 GPa10.2 Msi
Shear Modulus5 GPa0.73 Msi
Poisson's Ratio0.15
Tensile Strength (Ultimate)180 MPa26.1 ksi
Elongation at Break0.4%
Compressive Strength220 MPa31.9 ksi
Flexural Strength200 MPa29 ksi
Shear Strength30 MPa4.4 ksi
Fracture Toughness (K_IC)8 MPa·√m7.3 ksi·√in

Thermal5

C/C Composite 3D is rated for continuous service to 2,500°C (4,532 °F). It conducts heat at 50 W/m·K (28.9 BTU/hr·ft·°F), better than 70% of ceramic grades. Thermal expansion is 1 µm/m·K (0.556 µin/in·°F).

Thermal Conductivity50 W/m·K28.9 BTU/hr·ft·°F
Specific Heat Capacity710 J/kg·K0.17 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)1 µm/m·K0.56 µin/in·°F
Max Service Temperature (continuous)2,500°C4,532 °F
Min Service Temperature-200°C-328 °F

Electrical2

C/C Composite 3D has an electrical resistivity of 2×10⁻⁵ Ω·m.

Electrical Resistivity2×10⁻⁵ Ω·m787 µΩ·in
Volume Resistivity0 Ω·cm

Chemical & Environmental2

Corrosion resistance is very good (70/100), worse than 59% of ceramic grades.

Corrosion ResistanceVery good70/100
Chemical Resistance SummaryInert to nearly all acids, alkalis, molten salts and metals (except carbide formers and strong oxidizers); attacked by O2 above ~400 °C, by steam above ~700 °C and by HNO3/chromic acid — requires SiC or Si-based coating for hot-air service.

Sustainability4

Producing a kilogram of C/C Composite 3D takes about 750 MJ of energy and emits 55 kg of CO₂ — more than 96% of ceramic grades. Typical recycled content is 0%.

Embodied Energy (primary production)750 MJ/kg322,442 BTU/lb
Embodied Carbon (primary production)55 kg CO₂/kg
Embodied Water900 L/kg108 gal/lb
Typical Recycled Content0%

Manufacturability3

C/C Composite 3D's machinability is poor (25/100, better than 84% of ceramic grades).

MachinabilityPoor25/100
PolishabilityPoor20/100
Sintering / Firing Temperature2,200°C3,992 °F

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with C/C Composite 3D

Is C/C Composite easy to machine?

Machine dry with diamond/PCD or carbide tooling and strong dust extraction (respirable carbon dust); support laminates to avoid edge delamination and avoid interrupted cuts on coated parts.

Can C/C Composite be welded?

Not weldable — joints are made with carbonizable adhesives/carbon cement, graphite or C/C fasteners, or brazing to metals via SiC-coated interlayers.

Can C/C Composite be formed, bent or molded?

Net-shape is set at the preform stage (fabric layup, needled felt, 3D weaving) then densified by CVI or repeated resin/pitch impregnation-carbonisation cycles and graphitised at 2000–2800 °C; no post-forming is possible.

What surface finishes work on C/C Composite?

Purification (halogen gas at high temperature) for semiconductor grades, and CVD SiC / Si-slurry or pyrolytic-carbon sealing coats for oxidation protection above 450 °C; surfaces cannot be plated or painted conventionally.

C/C Composite chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
ash (impurities)purified grades for semiconductor use <20 ppm ash0 – 0.10.02
Si (coating, SiC-coated variant only)CVD SiC surface layer 50–200 µm, not part of bulk——
Ccarbon fiber reinforcement + pyrolytic/resin/pitch carbon matrix≥ 99 (balance)—

C/C Composite 3D — frequently asked

What is C/C Composite 3D used for?

C/C Composite 3D is typically used for aircraft brake discs, rocket nozzles, hot-zone furnace fixtures and semiconductor susceptors. In short: highest service temperature carbon; tougher than monolithic graphite; strongest carbon material here.

What is the tensile strength of C/C Composite 3D?

C/C Composite 3D has a typical tensile strength of 180 MPa (26.1 ksi) — stronger than 57% of ceramic grades. Strength varies by condition: see the 3 listed tempers.

Is C/C Composite 3D easy to machine?

Not especially — machinability is rated poor (25/100, better than 84% of ceramic grades). Machine dry with diamond/PCD or carbide tooling and strong dust extraction (respirable carbon dust); support laminates to avoid edge delamination and avoid interrupted cuts on coated parts.

Can C/C Composite 3D be welded?

Not weldable — joints are made with carbonizable adhesives/carbon cement, graphite or C/C fasteners, or brazing to metals via SiC-coated interlayers.

What surface finishes work on C/C Composite 3D?

Purification (halogen gas at high temperature) for semiconductor grades, and CVD SiC / Si-slurry or pyrolytic-carbon sealing coats for oxidation protection above 450 °C; surfaces cannot be plated or painted conventionally.

Can C/C Composite 3D be formed, bent or molded?

Net-shape is set at the preform stage (fabric layup, needled felt, 3D weaving) then densified by CVI or repeated resin/pitch impregnation-carbonisation cycles and graphitised at 2000–2800 °C; no post-forming is possible.

What is the maximum service temperature of C/C Composite 3D?

C/C Composite 3D is rated for continuous use to about 2,500°C (4,532 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Sources

  1. ASM Handbook Vol.21: Composites — Carbon-Carbon Composites — ASM International (2001)
  2. Carbon-Carbon Materials and Composites — Noyes / NASA RP-1254 (Buckley & Edie) (1993)
  3. SIGRABOND carbon fiber reinforced carbon — SGL Carbon (2022)
  4. CX/CC series carbon fiber composite for thermal field — Toyo Tanso (2021)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.