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Start | Lockheed Martin | F-16I Sufa


General information


ManufacturerLockheed Martin
ModelF-16I Sufa
ModificationF-16I
CountryUSA, Israel
Years2003
TypeFighter
Main rotor diameter-
Tail rotor diameter-
Wingspan9.45 m
Length15.03 m
Height5.09 m
Wing area27.87 m2
Zero fuel weight-
Empty weight8780 kg
Maximum takeoff weight-
Normal takeoff weight15200 kg
Flight duration-
Engine1 Ф Pratt Whitney F-100-PW-229
Power-
Thrust-
Maximum speed-
Cruising speed-
Rate of climb-
Practical range-
Service ceiling18500 m
Hovering ceiling-
Crew1
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