McDonnell Douglas F-4 Phantom II vs. PZL TS-11 Iskra

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McDonnell Douglas F-4 Phantom II versus PZL TS-11 Iskra
19.2 m 63 ft 0 in length 11.15 m 36 ft 7 in
5.03 m 16 ft 6 in height 3.5 m 11 ft 6 in
11.72 m 38 ft 5 in wingspan 10.06 m 33 ft
Two General Electric J79s engines 1 (WSK PZL Rzeszow SO-3W)
17,900 lbs thrust per engine 10.8 kN
35,800 lbs total thrust 10.8 kN
27,965 kg 61,700 lb MTOW 3,840 kg 8,466 lb
3,031 km 1,636 nm range 1,250 km 675 nm
Mach 2.2 2,717 km/h cruise speed 770 km/h 478 mph
Up to 16,000 lbs of externally carried ordnance 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.