McDonnell Douglas F-4 Phantom II vs. Scottish Aviation T1 Bulldog
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| McDonnell Douglas F-4 Phantom II |
versus |
Scottish Aviation T1 Bulldog |
| 19.2 m |
63 ft 0 in |
length |
7.11 m |
23 ft 4 in |
| 5.03 m |
16 ft 6 in |
height |
2.08 m |
6 ft 10 in |
| 11.72 m |
38 ft 5 in |
wingspan |
10.21 m |
33 ft 6 in |
| Two General Electric J79s |
engines |
1 x Lycoming O-360-A4M piston engine |
| 17,900 lbs |
thrust per engine |
Approximately 180 hp |
| 35,800 lbs |
total thrust |
Approximately 180 hp |
| 27,965 kg |
61,700 lb |
MTOW |
1,111 kg |
2,450 lb |
| 3,031 km |
1,636 nm |
range |
1,050 km |
567 nm |
| Mach 2.2 |
2,717 km/h |
cruise speed |
222 km/h |
138 mph |
| Up to 16,000 lbs of externally carried ordnance |
capacity |
Instructor pilot and one student |
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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.
