Bombardier CRJ1000 vs. Lockheed Ventura
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Bombardier CRJ1000 |
versus |
Lockheed Ventura |
39.1 m |
128 ft 5 in |
length |
15.7 m |
51 ft 5 in |
7.5 m |
24 ft 7 in |
height |
3.6 m |
11 ft 10 in |
26.2 m |
86 ft |
wingspan |
20 m |
65 ft 7 in |
2 GE CF34-8C5A1 turbofans |
engines |
2 x Pratt & Whitney R-2800 radial 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 |
2,000 hp |
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 |
4,000 hp |
41,640 kg |
91,800 lb |
MTOW |
15,000 kg |
33,100 lb |
3,004 km |
1,623 nm |
range |
2,670 km |
1,440 nmi |
515 mph |
829 km/h |
cruise speed |
230 mph |
370 km/h |
100 (common) |
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.