Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Northrop Grumman R-BAT Military Unmanned Helicopter System (UHS).
1 x Yamaha 2-cylinder, 2-stroke water-cooled engine driving a two-bladed main rotor and a two-bladed tail rotor.
Propulsion
6,004 ft
1,830 m | 1 miles
Service Ceiling