spacecraft reentry electrically charged plasma thermal protection system

when a spacecraft reenters the atmosphere 

then friction from the atmosphere creates a plasma 

that surrounds the lower part of the spacecraft 

usually the space shuttle needs a thermal protection system 

made of heat tiles 

according to media, the atmospheric plasma is neutrally charged

but if the space shuttle instead could use electricity or other energy 

to add or remove electrons to the atmospheric plasma 

then the atmospheric plasma could be positively or negatively charged

and then electromagnets inside the spacecraft 

could control the charged atmospheric plasma 

to use it as a heat shield 

if the spacecraft absorbs heat from reentry into atmosphere 

then that heat could accelerate fluid inside a closed system turbine 

to generate electricity 

and that electricity could be used to add or remove electrons to the atmospheric plasma 

and power the electromagnets controlling the atmospheric plasma