Conceptualization of design modifications in re-entry vehicles - vectoring for redirection of plasma

INIS

• plasma 100%
• design 100%
• modifications 100%
• reentry vehicles 100%
• mars planet 80%
• laboratories 60%
• surfaces 40%
• speed 40%
• vehicles 40%
• propulsion 40%
• cones 40%
• reentry 40%
• safety 20%
• increasing 20%
• data 20%
• phenols 20%
• values 20%
• velocity 20%
• probability 20%
• atmospheres 20%
• dynamics 20%
• density 20%
• vectors 20%
• adjustments 20%
• shear 20%
• nozzles 20%
• drag 20%
• trajectories 20%
• carbon 20%
• symmetry 20%
• wind 20%
• diffusers 20%
• jets 20%
• drag coefficient 20%
• shields 20%
• nasa 20%
• temperature gradients 20%
• shock waves 20%
• boundary layers 20%
• kinetic energy 20%
• space vehicles 20%

Physics

• Revisions 100%
• Reentry Vehicle 100%
• Area 40%
• Coefficients 40%
• Vehicle 40%
• Propulsion 40%
• Drag 40%
• Angle of Attack 40%
• Landing 40%
• Reentry 40%
• Mars 40%
• Turbulent Boundary Layer 40%
• Mars Science Laboratory 40%
• Technology 20%
• Degradation 20%
• Safety 20%
• Value 20%
• Independent Variables 20%
• Speed 20%
• Diameters 20%
• Increasing 20%
• Boundaries 20%
• Adjusting 20%
• Probability Theory 20%
• Sensory Perception 20%
• Shears 20%
• Hypersonics 20%
• High Speed 20%
• Ballistics 20%
• Supersonics 20%
• Temperature Gradients 20%
• Spacecraft 20%
• Kinetic Energy 20%
• Planetary Atmosphere 20%
• Ablative Materials 20%
• Hypersonic Speed 20%

Engineering

• Design 100%
• Conceptualization 100%
• Redirection 100%
• Re-Entry Vehicle 100%
• Laboratories 60%
• Surfaces 40%
• Obtains 40%
• Angle-of-Attack 40%
• Landing 40%
• Development 20%
• Density 20%
• Vectors 20%
• Nozzle 20%
• Energy Engineering 20%
• Trajectories 20%
• Velocity 20%
• Diffusers 20%
• Kinetic 20%
• Drag Coefficient 20%
• High Speed 20%
• Directional 20%
• Phenolics 20%
• Temperature Gradient 20%
• Payload 20%
• Spacecraft 20%
• Jet Propulsion 20%
• NASA 20%
• Shockwave 20%
• Impregnated Carbon 20%
• Hypersonic Speed 20%
• Wind Shear 20%