2-Blade Catto (Gen 2) Data
Flight test derived data, RV-4 s/n 2112 (short gear). 983 lb operating weight, CG @ 69.83" aft of Van's standard datum. Operating weight includes unusable fuel, all equipment and furnishings (i.e., everything except crew boarding weight). Aircraft fitted with Lycoming O-320-D2J (160 hp) engine (certified configuration + fuel pump, carburetor equipped), Vetterman four-pipe exhaust system and standard Van's cowl and baffle system. A Catto two-blade (second generation) prop is installed. Nickel leading edges. 68 x 72. Data is for "prop out of the box," i.e., no post-manufacture tweaks by Craig. The prop was designed to achieve 195 MPH Vmax at 2700 RPM at 8000 density altitude. When reviewing the tables, use CAS and or TAS (not IAS) for comparison purposes data is presented in MPH and Knots. Sorry, but I don't have data for high-altitude cruise. Above 8-10K', TAS becomes the primary reference to ensure I'm not encroaching on Vne (210 MPH)--especially during descent.
Like Smokey said, YMMV! I imagine that the Gen 3 Catto will be an outstanding fixed-pitch propeller; but expect the improvements to be in the area of takeoff/climb performance and, perhaps, cooling flow--i.e., even better all-around performance...I'll defer to Smokey and Axel's comments...The current Catto prop is more than capable of nailing specified cruise performance!
First table is Lycoming-derived power available vs. altitude:
Second table is climb/glide data:
Third table is cruise performance data with gear leg fairings and wheel pants installed:
Fourth table is cruise data, wheel pants removed (winter operations, etc.)--note gear leg fairings remain installed:
Fly safe,
Vac