Gathering parts to build a "table top" demo assembly for tail rotor failur recovery set up. It will have a main fixed pitch rotor hub and tail boom w/ an electric TR that I can shut off to cause the torque to "Peg" the tail boom in one direction representing catostrophic failure. If I can engage the recovery assembly and cause the tail boom to stay between two "pegs" 180 degrees apart it will at least be better than "spinning to doom" and crashing. Even "fish tailing" or long drawn out airframe spin in a tight orbit may allow enough control to get it to the ground with out the "sudden" stop and die syndrome. We'll see. I'm behind on all my projects due to the holidays and the Army taking up my time. Boxing the CF prototype and taking it home over Xmas leave and try to finish it and get it to fly. Aluminum airframe will reflect the patent drawings..........single vertical down tube is being replaced with dual down tube/struts. More to follow.