| Název: Name: | Lockheed Martin F-16I Sufa | Lockheed Martin F-16I Sufa |
| Originální název: Original Name: | Lockheed Martin F-16I Sufa | |
| Kategorie: Category: | bombardovací letoun | bomber aeroplane |
| Výrobce: Producer: | DD.MM.2003-DD.MM.2008 Lockheed Martin Corp., Fort Worth, Texas | |
| Období výroby: Production Period: | DD.MM.2003-DD.MM.2008 | |
| Vyrobeno kusů: Number of Produced: | 102 | |
| První vzlet: Maiden Flight: | 23.12.2003 | |
| Osádka: Crew: | 2 | |
| Základní charakteristika: Basic Characteristics: | ||
| Vzlet a přistání: Take-off and Landing: | CTOL - konvenční vzlet a přistání | CTOL - conventional take-off and landing |
| Uspořádání křídla: Arrangement of Wing: | jednoplošník | monoplane |
| Uspořádání letounu: Aircraft Concept: | klasické | conventional |
| Podvozek: Undercarriage: | zatahovací | retractable |
| Přistávací zařízení: Landing Gear: | kola | wheels |
| Technické údaje: Technical Data: | ||
| Hmotnost prázdného letounu: Empty Weight: | 8809 kg | 19420 lb |
| Vzletová hmotnost: Take-off Weight: | ? kg | ? lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 23587 kg | 52000 lb |
| Rozpětí: Wingspan: | 9.45 m | 31ft |
| Délka: Length: | 15.04 m | 49ft 4in |
| Výška: Height: | 5.09 m | 16ft 8.5in |
| Plocha křídla: Wing Area: | 27.87 m2 | 300 ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | dvouproudový | turbofan |
| Počet motorů: Number of Engines: | 1 | |
| Typ: Type: | Pratt & Whitney F100-PW-229 - maximální tah s přídavným spalováním: 129,44 kN | Pratt & Whitney F100-PW-229 - maximum thrust, afterburning: 29100 lbf |
| Objem palivových nádrží: Fuel Tank Capacity: | trup + křídlo: 3297 l přítrupové nádrže: 1703 l | fuselage + wing: 871 US gal / 726 Imp gal conformal fuel tanks: 450 US gal / 375 Imp gal |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 2145 km/h v 12192 m | 1333 mph in 40000 ft |
| Cestovní rychlost: Cruise Speed: | ? km/h v ? m | ? mph in ? ft |
| Rychlost stoupání: Climb Rate: | ? m/s | ? ft/min |
| Čas výstupu na výšku: Time to Climb to: | ? min do ? m | ? min to ? ft |
| Operační dostup: Service Ceiling: | 18288+ m | 60000+ ft |
| Dolet: Range: | 12881) km | 8001) mi |
| Maximální dolet: Maximum Range: | ? km | ? mi |
| Výzbroj: Armament: | rotační kanón M61A1 Vulcan se zásobou ? kusů munice maximální hmotnost výzbroje 7700+ kg na 11 závěsnících střely: 6x AIM-9L Sidewinder 6x AIM-120 AMRAAM 6x Python 4 6x Python 5 6x Derby 4x Delilah pumy: 4x Mk.84 8x Mk.83 12x Mk.82 4x GBU-15/B 4x GBU-16/B 4x GBU-31/B 8x GBU-39/B 4x Spice ostatní: AN-AAQ-13 LANTIRN Litening | M61A1 Vulcan gatling gun with ? rounds of ammunition maximum armament weight of 17000+ lb on 11 hardpoints missiles: 6x AIM-9L Sidewinder 6x AIM-120 AMRAAM 6x Python 4 6x Python 5 6x Derby 4x Delilah bombs: 4x Mk.84 8x Mk.83 12x Mk.82 4x GBU-15/B 4x GBU-16/B 4x GBU-31/B 8x GBU-39/B 4x Spice other: AN-AAQ-13 LANTIRN Litening |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | 1) bez doplňování paliva za letu | 1) without in-flight refueling |
| Zdroje: Sources: | - | |
Lockheed Martin F-16I Sufa
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Reklama
This post has not been translated to English yet. Please use the TRANSLATE button above to see machine translation of this post.
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This post has not been translated to English yet. Please use the TRANSLATE button above to see machine translation of this post.
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This post has not been translated to English yet. Please use the TRANSLATE button above to see machine translation of this post.
Stroj nese nádrže 2 x 600 gal pod křídly, 1 x 300 gal pod trupem, střely Delilah AL pod křídly, kontejnery Litening a navigační AN/AAQ-13 LANTIRN pod trupem, cvičné střely Python-4 na koncích křídel.
Kecskemét 7. 8. 2010
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Reklama
A swarm of aircraft F-16I Sufa (493, 499, 437 and 403) of the armaments 119. squadron, may 2011.
Source: Israel Defense Forces
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