McDonnell Douglas F-4 Phantom II vs. Northrop T-38 Talon
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McDonnell Douglas F-4 Phantom II |
versus |
Northrop T-38 Talon |
19.2 m |
63 ft 0 in |
length |
14.1 m |
46 ft 4 in |
5.03 m |
16 ft 6 in |
height |
3.9 m |
12 ft 10 in |
11.72 m |
38 ft 5 in |
wingspan |
7.7 m |
25 ft 3 in |
Two General Electric J79s |
engines |
Two General Electric J85-GE-5A turbojet engines |
17,900 lbs |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
35,800 lbs |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
27,965 kg |
61,700 lb |
MTOW |
12,093 lb |
5,485 kg |
3,031 km |
1,636 nm |
range |
1,759 km |
950 nm |
Mach 2.2 |
2,717 km/h |
cruise speed |
745 kts |
1,380 km/h |
Up to 16,000 lbs of externally carried ordnance |
capacity |
Two (student and instructor) |
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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.