Numerical Analysis of Nozzle Cooling for Upper-stage Liquid Rocket Engines

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Topics

• Aircraft Engines
• Combustion Chambers
• Cooling Technology
• Heat Transfer
• Liquid-Propellant Rocket
• Nozzles
• Propulsion and Power
• Rocket Engine
• Rocket Propulsion
• Rocketry
• Thermal Control and Protection
• Thermophysics and Heat Transfer

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Keywords

• Nozzles
• Liquid Rocket Engine
• Heat Transfer Coefficients
• Combustion Chambers
• Regenerative Cooling
• Launch Vehicles
• Liquid Propellant Rocket Engine
• Numerical Analysis
• National Aerospace Laboratory of Japan
• Thermal Protection

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Digital

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Topics

• Aerospace Systems, Operations and Life Cycle