Lockheed F-104 Starfighter vs. North American B-25 Mitchell

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Lockheed F-104 Starfighter versus North American B-25 Mitchell
16.69 m 54 ft 9 in length 16.15 m 53 ft 0 in
4.11 m 13 ft 6 in height 5 m 16 ft 4 in
6.68 m 21 ft 11 in wingspan 20.58 m 67 ft 6 in
1 Turbojet Engine engines 2 x Wright R-2600-92 Twin Cyclone
46.7 / 71.2 kN (dry/with Afterburner) thrust per engine 1,700 horsepower
46.7 / 71.2 kN (dry/with Afterburner) total thrust 3,400 horsepower
13,500 kg 29,800 lb MTOW 7,484 kg 16,500 lb
1,200 km 648 nm range 1,350 mi 1,175 nm
510 mph 821 km/h cruise speed 233 MPH 375 km/h
capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.