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3D High Density Carbon Carbon Composite

Carbon Carbon Nozzles and Throat

High density C/C material

Fiber volume percent:          40-45%
Fiber volume percent hoop:     45% ± 5
Fiber volume percent axial:    36% ± 4
Fiber volume percent radial:   19% ± 4
Bulk density:                 ≥ 1.9     (g/cm )
Tensile strength (hoop):      ≥ 100      MPa
Tensile strength (axial):     not tested      MPa
Compressive strength (hoop):  ≥ 80       MPa
Compressive strength (axial): ≥ 71       MPa
Thermal conductivity (hoop):  ≥ 40       W/m.K  at 900 °C
Thermal conductivity (axial): ≥ 22       W/m.K  at 900 °C
Thermal expansion:            < 3.1      1/ºC*10 -6
Open porosity:                < 5%
Carbon Content:                 99.9%
Graphitization Temperature:   @ 2500 °C

What is feature of missile carbon carbon composite throat?

The carbon-carbon composite throat in missile technology is a critical component used in the nozzle section of rocket and missile engines. These throats are subjected to extremely harsh conditions, including high temperatures, corrosive gases, and intense pressures during rocket engine operation. The use of carbon-carbon composites in this application offers several distinct advantages:

Key Features of Carbon-Carbon Composite Throat

  1. High Temperature Resistance:

    • Durability at Extreme Temperatures: Carbon-carbon composites maintain structural integrity under extremely high temperatures (exceeding 2,500 degrees Celsius), which are typical in rocket engine nozzles.
    • Thermal Stability: They exhibit minimal thermal expansion at high temperatures, ensuring consistent performance and dimensional stability of the nozzle throat during operation.
  2. High Thermal Conductivity:

    • Efficient Heat Dissipation: The composite facilitates efficient heat dissipation, protecting the structure of the missile and enhancing the overall effectiveness of the cooling system.
  3. Erosion and Ablation Resistance:

    • Resilient to Ablation: The material resists ablation caused by the high-speed flow of hot gases, a common challenge in the throat area of missile nozzles.
    • Resistance to Chemical Attack: Carbon-carbon composites are resistant to the corrosive effects of the combustion gases and propellant chemicals.
  4. Strength and Lightweight:

    • High Strength-to-Weight Ratio: The composites provide considerable strength without adding significant weight, a critical factor in aerospace applications where weight reduction is paramount.
    • Mechanical Strength: Despite the high temperatures and corrosive environment, carbon-carbon composites maintain excellent mechanical strength.
  5. Fatigue Resistance:

    • Withstands High Pressure and Vibration: The material is capable of withstanding the cyclic loads and vibrations experienced during rocket engine operation, which helps in maintaining the integrity and alignment of the engine components.

Application Benefits

  • Enhanced Performance: The use of carbon-carbon composite throats helps in achieving higher thrust levels by allowing engines to operate at higher temperatures and pressures.
  • Longevity and Reliability: These materials reduce the need for frequent replacements due to their enhanced durability and erosion resistance.
  • Cost-Effectiveness: Although the initial cost may be high, the longer lifespan and reduced maintenance requirements offer long-term savings.

Carbon-carbon composite throats are an example of advanced materials engineering providing substantial benefits in demanding aerospace applications, particularly in improving the performance and reliability of missile technology.