Airbus A321XLR vs. Lockheed Martin F-35 Lightning II
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Airbus A321XLR |
versus |
Lockheed Martin F-35 Lightning II |
44.51 m |
146 ft 0 in |
length |
15.67 m |
51 ft 4 in |
11.76 m |
38 ft 7 in |
height |
4.33 m |
14 ft 2 in |
35.8 m |
117 ft 5 in |
wingspan |
10.7 m |
35 ft 1 in |
CFM LEAP-1A and P&W PW1100G |
engines |
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 |
33,000 lbs (147 kN) |
thrust per engine |
40,000 lb |
66,000 lbs (294 kN) |
total thrust |
40,000 lb |
101,000 kg |
222,700 lb |
MTOW |
31,800 kg |
70,000 lb |
4,700 nmi |
8,704 km |
range |
1,380 mi |
1,200 nm |
963km/h |
598mph |
cruise speed |
520 kt |
302 mph |
180-220 seats (typical 2-class seating) |
capacity |
18,000 pounds of total ordinance |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.