Shock Characteristics and Protective Design of Equipment During Spacecraft Docking Process

Engineering

• Shock Loads 100%
• Avionics 100%
• Docking 100%
• Sinusoidal Vibration 66%
• Obtains 33%
• Finite Element Modeling 33%
• Vibration Isolation 33%
• Dynamic Response 33%
• Adaptability 33%
• Spring Stiffness 33%
• Damping Coefficient 33%
• Mating Surface 33%
• Structural Damage 33%
• Resonance Frequency 33%
• Relative Speed 33%
• Frequency Error 33%

Material Science

• Electronic Component 100%
• Spacecraft 100%
• Avionics 60%
• Shock Loads 60%
• Finite Element Modeling 20%

Physics

• Spacecraft Docking 100%
• Spacecraft Electronic Equipment 25%