Lockheed F-104 Starfighter vs. McDonnell Douglas F-4 Phantom II

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Lockheed F-104 Starfighter versus McDonnell Douglas F-4 Phantom II
16.69 m 54 ft 9 in length 19.2 m 63 ft 0 in
4.11 m 13 ft 6 in height 5.03 m 16 ft 6 in
6.68 m 21 ft 11 in wingspan 11.72 m 38 ft 5 in
1 Turbojet Engine engines Two General Electric J79s
46.7 / 71.2 kN (dry/with Afterburner) thrust per engine 17,900 lbs
46.7 / 71.2 kN (dry/with Afterburner) total thrust 35,800 lbs
13,500 kg 29,800 lb MTOW 27,965 kg 61,700 lb
1,200 km 648 nm range 3,031 km 1,636 nm
510 mph 821 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.