Combined chemical-electric propulsion for a stand-alone mars Cubesat

INIS

• balances 16%
• capture 16%
• control 16%
• design 33%
• efficiency 16%
• fuels 16%
• hybrids 16%
• impulse 16%
• iodine 16%
• ion thrusters 16%
• mars planet 100%
• optimization 16%
• orbits 50%
• performance 66%
• power 16%
• power input 16%
• propellants 50%
• propulsion 100%
• propulsion systems 33%
• radiowave radiation 16%
• solutions 16%
• stabilization 16%
• thrusters 33%
• trajectories 50%
• variations 16%
• yields 16%

Engineering

• Active Distribution Network 25%
• CubeSat 100%
• Design 50%
• Electric Propulsion 100%
• Electrical System 25%
• Input Power 25%
• Models 50%
• Optimization 25%
• Orbital Transfer 25%
• Performance Characteristic 25%
• Propellant Mass 50%
• Propulsion System 50%
• Specific Impulse 25%
• Thruster 75%