Lockheed Martin F-35 Lightning II vs. Canadair CL-415
... or view the full comparison list
here.
Lockheed Martin F-35 Lightning II |
versus |
Canadair CL-415 |
15.67 m |
51 ft 4 in |
length |
19.82 m |
65 ft 0 in |
4.33 m |
14 ft 2 in |
height |
8.66 m |
28 ft 5 in |
10.7 m |
35 ft 1 in |
wingspan |
28.6 m |
93 ft 1 |
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 |
engines |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
40,000 lb |
thrust per engine |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
40,000 lb |
total thrust |
4,300 to 4,760 shaft horsepower |
31,800 kg |
70,000 lb |
MTOW |
19,733 kg |
43,525 lb |
1,380 mi |
1,200 nm |
range |
1,600 km |
864 nm |
520 kt |
302 mph |
cruise speed |
290 km/h |
180 mph |
18,000 pounds of total ordinance |
capacity |
|
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.