Experiment and semi-empirical modeling of lab-scale hybrid rocket performance

Keyphrases

• Poly(methyl methacrylate) 100%
• Chamber Pressure 100%
• Hydroxyl-terminated Polybutadiene 100%
• Hybrid Rocket 100%
• Semi-empirical Modeling 100%
• Rocket Performance 100%
• Hybrid Rocket Motor 100%
• Simplified Model 50%
• Combustion Temperature 50%
• Combustion 50%
• Time-resolved 50%
• Inertia 50%
• Equilibrium Analysis 50%
• Oxidizer 50%
• System Design 50%
• Combustion System 50%
• Operating Parameters 50%
• Design Parameters 50%
• Regression Rate 50%
• Mass Conservation 50%
• Parameter Optimization 50%
• Gaseous Oxygen 50%
• Flow Chamber 50%
• Rate Correlation 50%
• Nozzle Throat Diameter 50%
• Output Parameters 50%
• Combustion Parameters 50%
• Function Series 50%
• Characteristic Velocity 50%
• Linear Regression Rate 50%
• Semi-empirical Predictive Model 50%
• Temperature Effectiveness 50%
• Hybrid Combustion 50%

Engineering

• Chamber Pressure 100%
• Design Parameter 50%
• Experimental Result 50%
• Combustion Temperature 50%
• Rocket Engine 50%
• Oxidizer 50%
• NASA 50%
• Operating Parameter 50%
• Conservation of Mass 50%
• Characteristic Velocity 50%
• Parametric Optimization 50%
• Output Parameter 50%
• Hybrid Rocket Engine 50%