Hi hawkstriker512,
Have you posted on
rcgroups.com? They have lots of discussions on that. (I can probably jump in on your thread if you want me to.)
The first thing you need to figure out is your wing loading ratio. In straight and level flight (no wind) you can maintain altitude for a certain weight of solar panels that generate X watts/square meter only if your wing design can generate enough lift for that watt output at the propeller. You should derate by a significant percentage for: conversion of sunlight to electricity when the sun is not straight overhead, conversion from electricity to prop rotation, and conversion from prop rotation to thrust.
Post over on
rcgroups.com and they will be able to help you do the math.