Reliability based design optimization of a CubeSat de-orbiting mechanism

Engineering

• CubeSat 100%
• Design Optimization 100%
• Aerodynamic Drag 100%
• Reliability Based Design 100%
• Thin Membrane 100%
• System Component 50%
• Optimum Design 50%
• Multiobjective Optimization Problem 50%
• Simulation Method 50%
• Optimal Design 50%
• Solar Radiation 50%
• Drag Force 50%
• Manufacturing Quality 50%
• Maximum Lifetime 50%
• Probabilistic Design 50%
• Reliability Evaluation 50%
• Design Parameter 50%
• Pareto Optimal 50%

Keyphrases

• Deorbiting 100%
• Reliability-based Design Optimization 100%
• CubeSat 100%
• Spiral Spring 100%
• Thin Membrane 40%
• Orbit Decay 40%
• Atmospheric Density 40%
• Design Parameters 20%
• System Components 20%
• Optimization Framework 20%
• Optimization Criterion 20%
• Optimum Design 20%
• Aerodynamic Drag 20%
• Multi-objective Optimization Problem 20%
• Solar Radiation 20%
• In-house Code 20%
• Manufacturing Quality 20%
• Space Environment 20%
• Optimization Variables 20%
• Decay Process 20%
• Aerodynamic Drag Force 20%
• Membrane Structure 20%
• Monte Carlo Simulation Method 20%
• Producing Mechanism 20%
• Deterministic Optimization 20%
• Pareto Optimal Design 20%
• Time Criterion 20%
• Probabilistic Design 20%
• Maximum Lifetime 20%
• Reliability Evaluation 20%
• Satellite Tool Kit 20%
• Satellite Structure 20%
• Braking 20%
• Aero 20%