Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Boeing FARA Compound Helicopter Proposal.
1 x General Electric Aviation XT901 turboshaft engine developing 3,000 horsepower each driving a six-bladed main rotor unit, four-bladed tail rotor unit (facing port side), and four-bladed propulsor unit in "pusher" configuration.
Propulsion
202 mph
325 kph | 175 kts
Max Speed
14,764 ft
4,500 m | 3 miles
Service Ceiling
1,383 miles
2,225 km | 1,201 nm
Operational Range
1,000 ft/min
305 m/min
Rate-of-Climb