McDonnell Douglas F-4 Phantom II vs. Canadair CL-415
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McDonnell Douglas F-4 Phantom II |
versus |
Canadair CL-415 |
19.2 m |
63 ft 0 in |
length |
19.82 m |
65 ft 0 in |
5.03 m |
16 ft 6 in |
height |
8.66 m |
28 ft 5 in |
11.72 m |
38 ft 5 in |
wingspan |
28.6 m |
93 ft 1 |
Two General Electric J79s |
engines |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
17,900 lbs |
thrust per engine |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
35,800 lbs |
total thrust |
4,300 to 4,760 shaft horsepower |
27,965 kg |
61,700 lb |
MTOW |
19,733 kg |
43,525 lb |
3,031 km |
1,636 nm |
range |
1,600 km |
864 nm |
Mach 2.2 |
2,717 km/h |
cruise speed |
290 km/h |
180 mph |
Up to 16,000 lbs of externally carried ordnance |
capacity |
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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.