F/A-259 Striker
Specifications
| Variant | F/A-259 Strike | |
| Role | light attack | |
| Country | Czechia + Israel | |
| Builder | Aero Vodochody + Israel Aerospace Industries (IAI) | |
| First Flight | ||
| Status | development | |
| Number built | ||
| Operators | ||
| Cost | ||
| Comparable Aircraft | L139 | |
| Recognition | ||
| Wingspan | 9.75 meters | feet |
| Sweep | ||
| Wing Aspect Ratio | ||
| Fuselage Maximum Diameter | meters | 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 Plant | Honeywell 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 |
