boost phase interception depends on the large IR signature of a booster, not its radar cross section on any plasma sheath around an object in reentry.
Great, how is the onboard sensor of any reentry vehicle at 2000+ C degrees going to see a much smaller plume hidden behind the rest of a rocket, with no way to correct for distance since it is looking top down and IR sensors don't get to benefit from Doppler shift measurements like radar?
Even if it could what material is IR transparent and yet can survive 2000+ C? While understanding that IR transparency applies to the sensor as well, which means sensor is exposed to 2000+ C IR radiation?
Simple answer - it can't.