Commonwealth CA-25 Winjeel vs. McDonnell Douglas F-4 Phantom II
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Commonwealth CA-25 Winjeel |
versus |
McDonnell Douglas F-4 Phantom II |
7.77 m |
25 ft 6 in |
length |
19.2 m |
63 ft 0 in |
2.84 m |
9 ft 4 in |
height |
5.03 m |
16 ft 6 in |
10.82 m |
35 ft 6 in |
wingspan |
11.72 m |
38 ft 5 in |
1 x Pratt & Whitney R-985-AN-2 radial engine |
engines |
Two General Electric J79s |
Approximately 450 hp |
thrust per engine |
17,900 lbs |
Approximately 450 hp |
total thrust |
35,800 lbs |
5,650 lb |
2,563 kg |
MTOW |
27,965 kg |
61,700 lb |
1,287 km |
695 nm |
range |
3,031 km |
1,636 nm |
150 mph |
241 km/h |
cruise speed |
Mach 2.2 |
2,717 km/h |
Instructor pilot and one student |
capacity |
Up to 16,000 lbs of externally carried ordnance |
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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.