Lockheed P-2 Neptune vs. PZL TS-11 Iskra

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Lockheed P-2 Neptune versus PZL TS-11 Iskra
30.17 m 99 ft 0 in length 11.15 m 36 ft 7 in
10.15 m 33 ft 4 in height 3.5 m 11 ft 6 in
33.53 m 110 ft wingspan 10.06 m 33 ft
2 x Wright R-3350 radial engines engines 1 (WSK PZL Rzeszow SO-3W)
Approximately 3,700 hp thrust per engine 10.8 kN
Approximately 7,400 hp total thrust 10.8 kN
27,216 kg 60,000 lb MTOW 3,840 kg 8,466 lb
7,885 km 4,259 nm range 1,250 km 675 nm
300 mph 483 km/h cruise speed 770 km/h 478 mph
based on configuration capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.