Boeing 777-200ER vs. Northrop T-38 Talon
... or view the full comparison list
here.
Boeing 777-200ER |
versus |
Northrop T-38 Talon |
63.7 m |
209 ft 1 in |
length |
14.1 m |
46 ft 4 in |
18.6 m |
61 ft |
height |
3.9 m |
12 ft 10 in |
64.8 m |
212 ft 7 in |
wingspan |
7.7 m |
25 ft 3 in |
2 x GE90-115B |
engines |
Two General Electric J85-GE-5A turbojet engines |
115,300 lbf |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
230,600 lbf |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
286,897 kg |
632,500 lb |
MTOW |
12,093 lb |
5,485 kg |
13,649 km |
7,370 nmi |
range |
1,759 km |
950 nm |
Mach 0.84 |
1,037 km/h |
cruise speed |
745 kts |
1,380 km/h |
301 |
capacity |
Two (student and instructor) |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.