Bombardier CRJ1000 vs. North American F-100 Super Sabre
... or view the full comparison list
here.
| Bombardier CRJ1000 |
versus |
North American F-100 Super Sabre |
| 39.1 m |
128 ft 5 in |
length |
16.46 m |
54 ft 2 in |
| 7.5 m |
24 ft 7 in |
height |
4.93 m |
16 ft 2 in |
| 26.2 m |
86 ft |
wingspan |
11.84 m |
38 ft 1 |
| 2 GE CF34-8C5A1 turbofans |
engines |
1 Pratt & Whitney J57-P-21A |
| 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 |
16,000 lb. thrust in afterburner |
| 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 |
16,000 lb. (afterburner) |
| 41,640 kg |
91,800 lb |
MTOW |
17,609 kg |
38,800 lb |
| 3,004 km |
1,623 nm |
range |
2,673 km |
1,444 nm |
| 515 mph |
829 km/h |
cruise speed |
587 mph |
945 km/h |
| 100 (common) |
capacity |
|
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.
