McDonnell Douglas F-4 Phantom II vs. North American T-6 Texan
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McDonnell Douglas F-4 Phantom II |
versus |
North American T-6 Texan |
19.2 m |
63 ft 0 in |
length |
9.0 m |
29 ft 6 in |
5.03 m |
16 ft 6 in |
height |
3.56 m |
11 ft 8 in |
11.72 m |
38 ft 5 in |
wingspan |
12.8 m |
42 ft |
Two General Electric J79s |
engines |
1 x Pratt & Whitney R-1340-AN-1 radial engine |
17,900 lbs |
thrust per engine |
Approximately 600 hp |
35,800 lbs |
total thrust |
Approximately 600 hp |
27,965 kg |
61,700 lb |
MTOW |
5,617 lb |
2,548 kg |
3,031 km |
1,636 nm |
range |
1,175 km |
634 nm |
Mach 2.2 |
2,717 km/h |
cruise speed |
145 mph |
233 km/h |
Up to 16,000 lbs of externally carried ordnance |
capacity |
Pilot and one passenger |
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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.