Auster AOP.6 vs. McDonnell Douglas F-4 Phantom II

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Auster AOP.6 versus McDonnell Douglas F-4 Phantom II
7.24 m 23 ft 9 in length 19.2 m 63 ft 0 in
2.55 m 8 ft 4 in height 5.03 m 16 ft 6 in
10.97 m 36 ft wingspan 11.72 m 38 ft 5 in
1× de Havilland Gipsy Major 7 inline piston engines Two General Electric J79s
145 hp (108 kW) thrust per engine 17,900 lbs
145 hp (108 kW) total thrust 35,800 lbs
2,160 lb 980 kg MTOW 27,965 kg 61,700 lb
507 km 274 nm range 3,031 km 1,636 nm
174 km/h 108 mph cruise speed Mach 2.2 2,717 km/h
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.