Radiative transmission and absorption within the ablative heat shield of hypersonic vehicles

Engineering

• Wavelength 100%
• Experiment 100%
• Heat Shield 100%
• Hypersonic Vehicle 100%
• Codes 50%
• Energy Engineering 50%
• Facilities 50%
• Material Response 50%
• Response Code 50%
• System Protection 50%
• Coupled Model 50%
• Surface 50%
• Thermal Protection 50%
• Trajectory 50%
• Radiative Transfer Equation 50%
• Model 50%
• Radiant Heating 50%
• Heat Flux 50%

Physics

• Heat 100%
• Laser 100%
• Hypersonic Vehicle 100%
• Model 66%
• Response 66%
• Charring 66%
• Approximation 33%
• Radiative Transfer Equation 33%
• Heating 33%
• Vehicle 33%
• Validity 33%
• Protection System 33%
• Atmospheric Entry 33%
• Ablative Material 33%
• Reentry Trajectory 33%
• Pulse 33%
• Deposit 33%

Material Science

• Laser 100%
• Materials 100%
• Surface (Surface Science) 33%
• Ablative Material 33%