Grumman HU-16 Albatross vs. Lockheed Martin F-35 Lightning II

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Grumman HU-16 Albatross versus Lockheed Martin F-35 Lightning II
19.05 m 62 ft 10 in length 15.67 m 51 ft 4 in
7.87 m 25 ft 10 in height 4.33 m 14 ft 2 in
29.41 m 96 ft 6 in wingspan 10.7 m 35 ft 1 in
2 x Wright R-1820-76 Cyclone radial engines engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
Approximately 1,425 hp each thrust per engine 40,000 lb
Approximately 2,850 hp total total thrust 40,000 lb
33,000 lb 14,969 kg MTOW 31,800 kg 70,000 lb
4,442 km 2,398 nm range 1,380 mi 1,200 nm
155 mph 249 km/h cruise speed 520 kt 302 mph
Pilot, co-pilot, flight engineer, and crew chief capacity 18,000 pounds of total ordinance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.