Randy Haskin wrote:
Those contra-rotating props do a nice job of countering the torque, so probably not.
Sorry, the contra-rotating prop doesn't change the need for a larger vertical stabilizer.
Given an already flying airplane, a contra-rotating prop has a greater polar moment of inertia due to the increased blade area/mass. This requires a larger vertical stabilizer.
In Dreadnought's case, the prop is quite a bit farther forward than on a stock Sea Fury since the engine is longer. Since the polar moment of inertia acts on a longer moment arm, a larger vertical stabilizer is required to maintain the same stability. On the Super Corsair, the R-4360 was moved back quite a bit since the R-4360 has radially positioned accessories (like the Centaurus) while the R-2800 has them positioned behind the engine parallel to the crankshaft centerline. This kept the Super Corsair prop roughly in the same place.
Torque and P-Factor are neutralized with a contra-rotating prop however.
Griffon Spitfires (5-bladed props) cannot use full throttle on takeoff because they can't maintain directional control. Vertical stabilizer lift is not adequate at low speeds. Lift is a function of vertical stabilizer area, rudder size, and rudder deflection (and airspeed obviously).
In conclusion, the need for vertical stabilizer area depends on the polar moment of inertia of the prop and the prop's moment arm. That's to maintain adequate yaw stability. This can be balanced through the use of a larger area or a longer moment arm for the stabilizer. I think you'll find a longer tail on the MB-5 replica than on a Mustang.
Now a few comments about the MB-5 replica...
I watched John Marlin lay out the framework for the MB-5 replica in Chino. He kept it as close to original as he could given the use of Mustang parts and no engineering drawings. He had plenty of photos and other data to do the design, so I suspect that it is closer than some suspect. He retired from Rockwell (now Boeing) in the blueprint shop, so he had access to all the equipment required to scale up drawings and photos to the required size. He also enlisted the help of Bruce Boland as I recall for the basic aerodynamic design (i.e. stability and control calculations). This is a high powered homebuilt. I'm sure John will use a qualified test pilot for the initial flights and will not do the actual race piloting himself (at least he never did with his Mustang).