McDonnell Douglas F-4 Phantom II vs. Westland Lysander
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McDonnell Douglas F-4 Phantom II |
versus |
Westland Lysander |
19.2 m |
63 ft 0 in |
length |
9.3 m |
30 ft 6 in |
5.03 m |
16 ft 6 in |
height |
3.51 m |
11 ft 6 in |
11.72 m |
38 ft 5 in |
wingspan |
15.24 m |
50 ft |
Two General Electric J79s |
engines |
1 x Bristol Mercury XII radial engine |
17,900 lbs |
thrust per engine |
Approximately 870 hp |
35,800 lbs |
total thrust |
Approximately 870 hp |
27,965 kg |
61,700 lb |
MTOW |
7,500 lb |
3,402 kg |
3,031 km |
1,636 nm |
range |
966 km |
522 nm |
Mach 2.2 |
2,717 km/h |
cruise speed |
190 mph |
306 km/h |
Up to 16,000 lbs of externally carried ordnance |
capacity |
Pilot and observer |
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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.