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
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.