Lockheed Ventura vs. Northrop T-38 Talon

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Lockheed Ventura versus Northrop T-38 Talon
15.7 m 51 ft 5 in length 14.1 m 46 ft 4 in
3.6 m 11 ft 10 in height 3.9 m 12 ft 10 in
20 m 65 ft 7 in wingspan 7.7 m 25 ft 3 in
2 x Pratt & Whitney R-2800 radial engines engines Two General Electric J85-GE-5A turbojet engines
2,000 hp thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
4,000 hp total thrust 4,100 pounds dry thrust; 5,800 with afterburners
15,000 kg 33,100 lb MTOW 12,093 lb 5,485 kg
2,670 km 1,440 nmi range 1,759 km 950 nm
230 mph 370 km/h cruise speed 745 kts 1,380 km/h
capacity Two (student and instructor)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.