McDonnell Douglas F-4 Phantom II vs. Aero Commander 1000

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McDonnell Douglas F-4 Phantom II versus Aero Commander 1000
19.2 m 63 ft 0 in length 13.67 m 44 ft 10 in
5.03 m 16 ft 6 in height 3.75 m 12 ft 4 in
11.72 m 38 ft 5 in wingspan 15.02 m 49 ft 3 in
Two General Electric J79s engines 2 x Pratt & Whitney Canada PT6A-28
17,900 lbs thrust per engine 450 lbs
35,800 lbs total thrust 900 lbs
27,965 kg 61,700 lb MTOW 10,500 lb 4,763 kg
3,031 km 1,636 nm range 1,750 nm 3,241 km
Mach 2.2 2,717 km/h cruise speed 282 kts 175 mph
Up to 16,000 lbs of externally carried ordnance capacity Up to 8 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.