Northrop T-38 Talon vs. Robinson R22

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Northrop T-38 Talon versus Robinson R22
14.1 m 46 ft 4 in length 8.76 m 28 feet 75 inch
3.9 m 12 ft 10 in height 2.72 m 8 feet 9 inch
7.7 m 25 ft 3 in wingspan
Two General Electric J85-GE-5A turbojet engines engines 1 x Lycoming O-320
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 110 kW
4,100 pounds dry thrust; 5,800 with afterburners total thrust 110 kW
12,093 lb 5,485 kg MTOW 635 kg 1,400 lb
1,759 km 950 nm range 348 km 188 nm
745 kts 1,380 km/h cruise speed 177 km/h 110 mph
Two (student and instructor) capacity 1 pilot + 1 passenger
rotor diameter 7.67 m 25 ft 2 in
rate of climb 5.2 m/s 1,024 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.