Bombardier CS300 vs. McDonnell Douglas F-4 Phantom II
... or view the full comparison list
here.
Bombardier CS300 |
versus |
McDonnell Douglas F-4 Phantom II |
38.0 m |
124 ft 7 in |
length |
19.2 m |
63 ft 0 in |
11.5 m |
37 ft 9 in |
height |
5.03 m |
16 ft 6 in |
35.1 m |
115 ft 2 in |
wingspan |
11.72 m |
38 ft 5 in |
2x Pratt & Whitney PurePower PW1000G |
engines |
Two General Electric J79s |
93.4 kN |
thrust per engine |
17,900 lbs |
186.8 kN |
total thrust |
35,800 lbs |
67,585 kg |
149,000 lb |
MTOW |
27,965 kg |
61,700 lb |
5,463 km |
2,952 nm |
range |
3,031 km |
1,636 nm |
871 km/h |
541 mph |
cruise speed |
Mach 2.2 |
2,717 km/h |
130 to 145 passengers |
capacity |
Up to 16,000 lbs of externally carried ordnance |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.