Frequently Asked Questions

 A kinetic propeller is a patent-pending propeller design that delivers superior aerodynamic performance across a wide range of flight speeds. Unlike conventional fixed-pitch or constant-speed propellers, the kinetic propeller maintains high efficiency from takeoff through cruise, with performance characteristics that improve as aircraft speed increases. 

There are numerous benefits, but some of the most important include higher cruise speeds, reduced emissions, longer range, higher climb rate and reduced noise.

To date, we have performed calculations, simulations and scale model tests. The collected data matches with predictions, however we still are going to do full scale ground tests to validate prior to pre-production flight tests.

 Innovation frequently involves applying known principles in new combinations. The kinetic propeller synthesizes established aerodynamic science in a configuration that has not previously been applied to propeller design. With a patent pending, we are confident the invention represents a genuinely novel approach. 

Besides reduced noise amplitude (volume), the frequency (pitch) of the kinetic propeller is in a less annoying range. But perhaps most important is the reduction in energy required for any given speed. An internal combustion aircraft will burn less fuel per hour resulting in lower emissions. An electric aircraft will see a vastly improved range over stock propellers.

Current electric aircraft suffer from short range and heavy batteries. Due to the weight sensitive nature of aviation, they simply do not offer enough benefit for serious long-range travel. While unable to create parity with internal combustion aircraft, a kinetic propeller will improve electric aircraft performance significantly. This should help reduce range anxiety among potential users. 

The great part about this design is that very few changes need to be made to match a propeller with any particular airframe. Initially, we will be focused on fixed-pitch piston and electric single engine aircraft. The pending FAA MOSAIC standards may simplify integration with existing certified aircraft types. Otherwise, we will eventually certify to comply with FAA Part 35. If Part 35 is required, it will be a long term goal as the testing requirements and budget will be substantial. 

 Full-scale ground testing is currently underway. Flight testing is planned to follow upon successful completion of ground validation. The primary bottleneck is capital to manufacture and instrument test components — we are actively pursuing funding partnerships to accelerate the timeline. As a safety-critical aerospace component, we will not rush the certification process.