Thermal modelling of E.S.A second young engineers satellite

Keyphrases

• Young Engineers 100%
• Reentry Capsule 100%
• Ejection System 100%
• Thermal Modeling 100%
• Spool 100%
• Control System 50%
• Steady State 50%
• Transfer Effects 50%
• Friction 50%
• High Temperature 50%
• Control Information 50%
• Data Systems 50%
• Major Components 50%
• Thermal Analysis 50%
• Support System 50%
• Power System 50%
• International Space Station 50%
• Deployer 50%
• Perigee 50%
• Swinging 50%
• Lumped Parameter Thermal Network 50%
• Mechanism System 50%
• Low-cost Hardware 50%
• Heat Dissipation 50%
• Ejection 50%
• Reentry 50%
• Thermal Design 50%
• Braking Mechanism 50%
• Control Power 50%
• Thermal Load 50%
• Momentum Transfer 50%
• Thermal Budget 50%
• Flight Direction 50%
• Thermal Network 50%
• Low Earth Orbit 50%
• Interface Constraint 50%

Engineering

• Control System 100%
• Nodes 100%
• Support System 100%
• Case Scenario 100%
• Network Model 100%
• Transients 100%
• Power Engineering 100%
• Heat Losses 100%
• Momentum Transfer 100%
• Major Component 100%
• Lumped Parameter 100%
• Final Application 100%
• State Case 100%
• Data Collection 100%
• Space Station 100%
• Low Earth Orbit 100%
• Thermal Load 100%

Physics

• Reentry 100%
• Thermal Design 100%
• Thermal Analysis 33%
• Data Control 33%
• Momentum Transfer 33%
• Cooling 33%
• Steady State 33%
• Data Acquisition 33%
• Earth Orbit 33%
• Transients 33%