Bombardier CRJ1000 vs. Lockheed P-2 Neptune

versus
... or view the full comparison list here.
Bombardier CRJ1000 versus Lockheed P-2 Neptune
39.1 m 128 ft 5 in length 30.17 m 99 ft 0 in
7.5 m 24 ft 7 in height 10.15 m 33 ft 4 in
26.2 m 86 ft wingspan 33.53 m 110 ft
2 GE CF34-8C5A1 turbofans engines 2 x Wright R-3350 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 Approximately 3,700 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 Approximately 7,400 hp
41,640 kg 91,800 lb MTOW 27,216 kg 60,000 lb
3,004 km 1,623 nm range 7,885 km 4,259 nm
515 mph 829 km/h cruise speed 300 mph 483 km/h
100 (common) capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.