Northrop T-38 Talon vs. Robinson R44 Raven II

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Northrop T-38 Talon versus Robinson R44 Raven II
14.1 m 46 ft 4 in length 11.66 m 38 ft 3 in
3.9 m 12 ft 10 in height 3.28 m 10 ft 9 in
7.7 m 25 ft 3 in wingspan
Two General Electric J85-GE-5A turbojet engines engines Lycoming IO-540-AE1A5
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 245 hp
4,100 pounds dry thrust; 5,800 with afterburners total thrust 245 hp
12,093 lb 5,485 kg MTOW 1,134 kg 2,500 lb
1,759 km 950 nm range 610 km 329 nm
745 kts 1,380 km/h cruise speed 222 km/h 138 mph
Two (student and instructor) capacity 3 passengers
rotor diameter 10.06 m 33 ft 0 in
rate of climb 5.1 m/s 1,000 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.