Fairey Gannet vs. Northrop T-38 Talon

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Fairey Gannet versus Northrop T-38 Talon
10.87 m 35 ft 8 in length 14.1 m 46 ft 4 in
3.76 m 12 ft 4 in height 3.9 m 12 ft 10 in
13.87 m 45 ft 6 in wingspan 7.7 m 25 ft 3 in
1 x Bristol Pegasus XVIII radial engine engines Two General Electric J85-GE-5A turbojet engines
Approximately 690 hp (515 kW) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Approximately 690 hp (515 kW) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
7,005 lb 3,178 kg MTOW 12,093 lb 5,485 kg
840 km 454 nm range 1,759 km 950 nm
139 mph 224 km/h cruise speed 745 kts 1,380 km/h
Pilot, Observer, and Air Gunner 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.