Composites · Carbon-matrix composites

Carbon–carbon composite

A carbon-fibre-reinforced carbon composite used where extreme temperature capability, low density and thermal-shock resistance outweigh oxidation sensitivity and cost.

Family
Carbon-Matrix Composite
Record
Standard
Conditions
1
Sources
3
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01

Overview

Material class
Composites
Category
Carbon-matrix composites
Family
Carbon-Matrix Composite
Product forms
Laminate/panel, Prepreg or semi-finished form (system dependent)

Composition

ConstituentMinMaxTypicalNote
Carbon fibrereinforcement architecture dependent
Carbon matrixpitch/resin/CVI route

02

Properties and conditions

Engineering properties

PropertyValueUnitCondition
Density~1.6–2.0g/cm³Representative; verify product form and condition
Temperature capability>2000°Cin inert/reducing environments
Thermal shock resistanceexcellentarchitecture dependent
Strength retentionhigh at temperatureoxidation protected
Oxidation resistancepoor without coatingair above ~500°C
Friction stabilityhighbrake grades

Conditions

reference

Representative system

Reinforcement, matrix, architecture, cure and environment must be stated.

03

Processing and use

Processing

  • Product form, thermal history and manufacturing route materially affect performance.

Applications

  • Aircraft brakes
  • Rocket nozzles
  • Re-entry thermal protection
  • Furnace fixtures

Selection considerations

  • Use the current governing standard and supplier certification for design or procurement.

04

Standards and related materials

Standards and designations

SystemDesignationNote
Aerospace/defence specificationcarbon–carbon compositeproduct-specific

05

Sources and context

Sources

Confirm the applicable specification, product form and condition before using values for design or procurement.

Supply and sustainability

Availability and lead time depend on grade, product form, certification and regional supply chain.

Segregated recovery and closed-loop recycling improve material efficiency where practical.