Northrop T-38 Talon vs. Kaman K-MAX

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Northrop T-38 Talon versus Kaman K-MAX
14.1 m 46 ft 4 in length 15.85 m 52.0 ft
3.9 m 12 ft 10 in height 4.10 m 13.5 ft
7.7 m 25 ft 3 in wingspan
Two General Electric J85-GE-5A turbojet engines engines 1 x Honeywell T53-17 turboshaft engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 1,600 hp
4,100 pounds dry thrust; 5,800 with afterburners total thrust 1,600 hp
12,093 lb 5,485 kg MTOW 2,721 kg 6,000 lb
1,759 km 950 nm range 370 km 200 nm
745 kts 1,380 km/h cruise speed 185 km/h 115 mph
Two (student and instructor) capacity 4.1
rotor diameter 13.2 m 43 ft 4 in
rate of climb 6.7 m/s 1,318 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.