A lunar cargo mission design strategy using variable low thrust

Engineering

• Transfer Trajectory 100%
• Trajectories 66%
• Continuous Variable 66%
• Thruster 66%
• Design 66%
• Characteristics 66%
• Spacecraft 66%
• Optimization Method 33%
• Optimisation Problem 33%
• Initial Condition 33%
• Computational Load 33%
• Design Technique 33%
• Optimal Trajectory 33%
• Numerical Method 33%
• Numerical Optimization 33%
• Propulsion System 33%
• Scoping Study 33%
• Basic Concept 33%

Physics

• Trajectory Optimization 66%
• The Moon 66%
• Mathematical Method 33%
• Geopotential 33%
• Interplanetary Flight 33%