Analysis of lithium-combustion power systems for extreme environment spacecraft

Keyphrases

• Power System 100%
• Extreme Environments 100%
• Mission Duration 66%
• Stirling Engine 66%
• Sulfur 33%
• Oxidizer 33%
• Venus 33%
• Dioxide 16%
• Lithium 16%
• Thermodynamics 16%
• Heat Transfer 16%
• Low Power 16%
• Total Mass 16%
• Closure Model 16%
• Thermal Energy 16%
• Battery Power 16%
• Time Constraints 16%
• Management Challenges 16%
• Power Output 16%
• Laboratory-based 16%
• Engineering Requirements 16%
• Heat Transfer Model 16%
• Earth Day 16%
• Limited Battery 16%
• Power-duration 16%
• Thermal Management 16%
• Engine Power 16%
• Lander 16%
• Potential Performance 16%
• Long-duration Mission 16%
• Sulfur Hexafluoride 16%

Engineering

• Power Engineering 100%
• Stirling Engine 66%
• Oxidizer 33%
• Sodium Sulfur Battery 33%
• Reactant 16%
• Engineering 16%
• Specifies 16%
• Power Output 16%
• Heat Transfer Model 16%
• Engine Power 16%
• Battery Power 16%
• Thermal Energy 16%