Purdue Propulsion Website

Useful Propulsion Data

Fundamental Properties of Internal Fluid Flows

• 1-D Isentropic Flow
  • Gamma=1.4
  • Gamma=1.3
  • Gamma=1.2
• Normal Shocks
• Fanno Flow
• Rayleigh Flow
• Rocket Thrust Coefficient Tables
  • Gamma=1.4
  • Gamma=1.3
  • Gamma=1.2
• U.S. Standard Atmosphere

Combustion and Thermochemical Data

• Specific Heat Data for Common Gases
• NASA Thermochemistry Code - Sample Input Files
• Heats of Formation and Chemical Composition
• Constant Pressure Equilibrium Constants (Kp Data)