Hi Rhett,
A couple of thoughts - as far as extending the spring length, a lot depends on the spring rate of the assembly itself - material, length, thickness, temper, etc., but I think you can run the risk of adding extra force & stress at the fuselage attach points because of the additional leverage. IMO, a thicker solid single leaf might not be good. Ideally with a tail spring, you want to match the spring rate of the main gear as close as possible - this can potentially improve 3 point landings. I've been intrigued with the solid rod (Whitman style) tailsprings, and curious if Lowell (Highwing) had any luck with his... maybe he will chime in.