Lockheed Ventura vs. McDonnell Douglas F-4 Phantom II

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Lockheed Ventura versus McDonnell Douglas F-4 Phantom II
15.7 m 51 ft 5 in length 19.2 m 63 ft 0 in
3.6 m 11 ft 10 in height 5.03 m 16 ft 6 in
20 m 65 ft 7 in wingspan 11.72 m 38 ft 5 in
2 x Pratt & Whitney R-2800 radial engines engines Two General Electric J79s
2,000 hp thrust per engine 17,900 lbs
4,000 hp total thrust 35,800 lbs
15,000 kg 33,100 lb MTOW 27,965 kg 61,700 lb
2,670 km 1,440 nmi range 3,031 km 1,636 nm
230 mph 370 km/h 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.