Dual Chemical-Electric Propulsion Systems Design for Interplanetary CubeSats

INIS

• design 100%
• propulsion systems 100%
• mars planet 100%
• space 100%
• trajectories 66%
• cost 66%
• propulsion 66%
• power 33%
• exploration 33%
• risks 33%
• hybrids 33%
• universities 33%
• solar system 33%
• optimization 33%
• impulse 33%
• capture 33%
• propellants 33%
• burns 33%
• size 33%
• orbits 33%
• emplacement 33%
• sizing 33%

Engineering

• CubeSat 100%
• Propulsion System 100%
• Electric Propulsion 100%
• Design 100%
• High Thrust 50%
• Requirement 50%
• Trajectory 50%
• Optimization 25%
• Electric Power Utilization 25%
• Limitations 25%
• Burn Time 25%
• Electrical System 25%
• Natural Resources Exploration 25%
• Low Cost 25%
• Space System 25%
• Design Parameter 25%
• Hybrid 25%
• High Risk 25%
• Propellant Mass 25%
• Specific Impulse 25%

Keyphrases

• Mission to Mars 50%
• Heuristic Optimization 50%
• Ballistic Capture 50%
• Solar System Exploration 50%
• Effective Space 50%
• In-situ Deployment 50%
• Low-thrust Trajectory 50%