Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Lockheed LMXT Aerial Refueling Tanker Aircraft Proposal.
2 x Rolls-Royce Trent 722B OR General Electric CF6-80E1A4 OR Pratt & Whitney PW4170 non-afterburning turbofan engines developing up to 72,000lb of thrust each unit.
Propulsion
637 mph
1,025 kph | 553 kts
Max Speed
42,700 ft
13,015 m | 8 miles
Service Ceiling
9,196 miles
14,800 km | 7,991 nm
Operational Range