Grumman OV-1 Mohawk vs. Canadair CL-415
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Grumman OV-1 Mohawk |
versus |
Canadair CL-415 |
12.52 m |
41 ft 1 in |
length |
19.82 m |
65 ft 0 in |
3.89 m |
12 ft 9 in |
height |
8.66 m |
28 ft 5 in |
14.63 m |
48 ft |
wingspan |
28.6 m |
93 ft 1 |
2 x Lycoming T53 turboprop engines |
engines |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
Approximately 1,100 hp each |
thrust per engine |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
Approximately 2,200 hp total |
total thrust |
4,300 to 4,760 shaft horsepower |
14,950 lb |
6,781 kg |
MTOW |
19,733 kg |
43,525 lb |
1,690 km |
913 nm |
range |
1,600 km |
864 nm |
230 mph |
370 km/h |
cruise speed |
290 km/h |
180 mph |
Pilot and observer |
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.