Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the LB-25-1 Heavy Bomber Design Study / Proposal.
4 x Wright R-3350 turbocharged air-cooled radial piston engines developing 2,200 horsepower each driving four-bladed propeller units in tractor arrangement.
Propulsion
391 mph
630 kph | 340 kts
Max Speed
32,005 ft
9,755 m | 6 miles
Service Ceiling
5,331 miles
8,580 km | 4,633 nm
Operational Range