A study of thermal radiation transfer in a solar thruster

Physics & Astronomy

• thrust 98%
• solar energy 98%
• thermal radiation 96%
• specific impulse 58%
• radiative heat transfer 54%
• convective heat transfer 52%
• propellants 49%
• energy absorption 49%
• emissivity 46%
• thermal energy 44%
• gases 44%
• nozzles 40%
• energy transfer 35%
• radiation 24%
• approximation 22%
• performance 19%
• temperature 12%

Engineering & Materials Science

• Heat radiation 100%
• Solar energy 79%
• Energy transfer 50%
• Particle size analysis 50%
• Gases 49%
• Energy absorption 47%
• Propellants 47%
• Thermal energy 43%
• Nozzles 37%
• Radiation 34%
• Heat transfer 29%
• Temperature 17%

Chemical Compounds

• Solar Energy 94%
• Radiative Heat Transfer 82%
• Convective Heat Transfer 72%
• Emissivity 61%
• Propellant 53%
• Nozzle 51%
• Gas 46%
• Dimension 33%
• Energy 20%