Bombardier CRJ1000 vs. Grumman OV-1 Mohawk
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Bombardier CRJ1000 |
versus |
Grumman OV-1 Mohawk |
39.1 m |
128 ft 5 in |
length |
12.52 m |
41 ft 1 in |
7.5 m |
24 ft 7 in |
height |
3.89 m |
12 ft 9 in |
26.2 m |
86 ft |
wingspan |
14.63 m |
48 ft |
2 GE CF34-8C5A1 turbofans |
engines |
2 x Lycoming T53 turboprop engines |
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve |
thrust per engine |
Approximately 1,100 hp each |
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve |
total thrust |
Approximately 2,200 hp total |
41,640 kg |
91,800 lb |
MTOW |
14,950 lb |
6,781 kg |
3,004 km |
1,623 nm |
range |
1,690 km |
913 nm |
515 mph |
829 km/h |
cruise speed |
230 mph |
370 km/h |
100 (common) |
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.