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I hope nobody at Northrop-Grumman is going "uh-oh" right now 
Here's an answer from our deputy project manager. Shielding from flares/CMEs will come from the spacecraft bus and the telescope itself. The sunshield structure will partially shadow the instrument module too and offer more shielding than the membranes will.
I guess since the buss below the shield could manage via dissipation.Just don’t know how the layers would interact with one another during an esd. Either way, thanks @NASAWebb & John for taking time to answer.
Webb rocks!
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JWST.
Given it will operate from L2, I have 2 questions.
1. Are there any methods through which JWST can avoid shield/mirror/system damage from micrometeorites ?
2. Are the layers able to protect the sensor from ionizing radiation from the sun (eg flares) ?
