Airbus A321-200 vs. Grumman OV-1 Mohawk
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Airbus A321-200 |
versus |
Grumman OV-1 Mohawk |
44.51 m |
146 ft 0 in |
length |
12.52 m |
41 ft 1 in |
11.76 m |
38 ft 7 in |
height |
3.89 m |
12 ft 9 in |
35.8 m |
117 ft 5 in |
wingspan |
14.63 m |
48 ft |
2 GE CFM56-5B3 |
engines |
2 x Lycoming T53 turboprop engines |
31,600 lbs |
thrust per engine |
Approximately 1,100 hp each |
63,200 lbs |
total thrust |
Approximately 2,200 hp total |
89,000 kg |
196,200 lb |
MTOW |
14,950 lb |
6,781 kg |
4,000 nmi |
7,408 km |
range |
1,690 km |
913 nm |
871 km/h |
541 mph |
cruise speed |
230 mph |
370 km/h |
185 to 220 |
capacity |
Pilot and observer |
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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.