Multi-objective design and trajectory optimization of space transport systems with RBCC propulsion via evolutionary algorithms and pseudospectral methods

Engineering

• Stages 100%
• Algorithm 66%
• Orbits 66%
• Mass Ratio 66%
• Combined Cycle 66%
• Fuel Mass 66%
• Design 33%
• Performance 33%
• Couplings 33%
• Optimization 33%
• Fuel 33%
• Hybrid 33%
• Minimization 33%
• Combines 33%
• Aerodynamic Performance 33%
• Low Altitude 33%
• Design Criterion 33%
• Dynamic Pressure 33%
• Design Optimization 33%
• Maximization 33%
• Specific Impulse 33%
• Combined-Cycle Engine 33%
• Maximum Altitude 33%

Physics

• Mach Number 100%
• Vehicle 100%
• Trajectory Optimization 100%
• Optimization 66%
• Algorithms 66%
• Mass Ratio 66%
• Design Optimization 66%
• Performance 33%
• Contrast 33%
• Parameter 33%
• Impact 33%
• Fuel 33%
• Transport System 33%
• Propulsion 33%
• Dynamic Pressure 33%
• Spectral Method 33%