Okay, you have my attention. What's the shape?
Better yet, give me a ballistic coefficient, L/D ratio and a nose radius. I'm assuming this is for lunar return. Are you assuming fixed angle-of-attack with roll modulation? If so then your trajectory would probably be a partial skip out to keep the G loading below 9 Gs followed by atmospheric return to parachute deployment that kept the heat flux near a constant optimal value. Are you assuming an ablator heat shield? Reusable heatshields don't exist for lunar return.
Gary
