Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Northrop N-1M Flying Wing Research Aircraft.
2 x Lycoming O-145 4-cylinder air-cooled piston engines developing 65 horsepower each (original); 2 x Franklin 6AC-264F2 6-cylinder air-cooled piston engines developing 117 horsepower each (later).
Propulsion
200 mph
322 kph | 174 kts
Max Speed
3,999 ft
1,219 m | 0 miles
Service Ceiling
300 miles
483 km | 261 nm
Operational Range
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).