Is the "V" strut setup really necessary if you just use low pressure tires for shock loads? Why couldn't you just insert a tube from where the V would normally attach and that would hold the gear from moving in or out. It would be less parts, so less weight, but I don't know if the change in geometry would adversely affect the fuselage.
is there any reason why this strut, along with cross cables will not work?
I believe the engineers will tell you that is a very weak gear for inboard side loads and will likely fail under minimal compression loads. also the close proximity of the brace strut to the main gear leg is high drag. the plans gear has been proven to be the most efficient for planes of our type and is difficult to improve. I installed a well thought out and executed carbon fiber low drag leaf gear on mine and the gain was near nil but the difficulty was way more than the plans gear.I will just follow the plans:) But it is fun to consider alternatives if she comes in heavy.