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Military


F/A-259 Striker

Specifications

VariantF/A-259 Strike
Rolelight attack
CountryCzechia + Israel
Builder Aero Vodochody +
Israel Aerospace Industries (IAI)
First Flight
Statusdevelopment
Number built
Operators
Cost
Comparable AircraftL139
Recognition
Wingspan 9.75 meters feet
Sweep
Wing Aspect Ratio
Fuselage Maximum Diametermeters feet
length 12.8 meters feet
height meters feet
wing area sqm sqfeet
Weight empty kg lb
takeoff (clean) kg lb
takeoff (maximum) 7,982 kg lb
Fuel, Internal kg lb
Fuel, External kg lb
Payload 2,722 kg lb
Max weapon load kg lb
Armament
Power PlantHoneywell F124-GA-100
Thrust, max, SLS, ISA 2,850 kg x lbst
Internal fuel (usable) kg lb
Performance (clean, ISA)
Max level speed (sea level) Mach 0.82
Limit speed KEAS / MN
Stall speed (landing, 20% fuel) KCAS
Stall speed (reference) KCAS
Rate of climb (SL) 52 m/s
Service ceiling meters feet
Range / 3 ext. tanks (10% reserve) km nm
Range, ext. tanks km nm
Range, clean km nm
Endurance, clean / ext. tanks h min / hr
Max sustained Load Factor (S.L.) g
Max sustained Load Factor (15,000 feet) +8 g and -4 g
Max sustained Turn Rate (15,000 feet) deg/sec
Takeoff ground run (S.L.) meters feet
Landing ground roll (S.L., 20% internal fuel) meters feet
Limit Load factor + g / - g
Crew
Accomodations




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Page last modified: 20-07-2018 05:32:03 ZULU