| Název: Name: | Northrop F-5N Tiger II | Northrop F-5N Tiger II |
| Originální název: Original Name: | Northrop F-5N Tiger II | |
| Kategorie: Category: | stíhací letoun | fighter aeroplane |
| Výrobce: Producer: | DD.MM.2003-DD.04.2009 Northrop Grumman Corporation, St. Augustine, Florida | |
| Období výroby: Production Period: | DD.MM.2003-DD.04.2009 | |
| Vyrobeno kusů: Number of Produced: | konverze z F-5E / conversion from F-5E: - 41 F-5N + 3 F-5F "FrankenTiger" | |
| První vzlet: Maiden Flight: | DD.03.2003 | |
| Osádka: Crew: | 1 | |
| 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: | ? kg | ? lb |
| Vzletová hmotnost: Take-off Weight: | ? kg | ? lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 11214 kg | 24722 lb |
| Rozpětí: Wingspan: | 8.13 m | 26ft 8in |
| Délka: Length: | 14.44 m | 47ft 4.7in |
| Výška: Height: | 4.07 m | 13ft 4.25in |
| Plocha křídla: Wing Area: | 17.28 m2 | 186 ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | jednoproudový | turbojet |
| Počet motorů: Number of Engines: | 2 | |
| Typ: Type: | General Electric J85-GE-21C o tahu 14,59 kN / 22,24 kN s přídavným spalováním | General Electric J85-GE-21C, thrust 3280 lb.st. / 5000 lb.s.t. with afterburning |
| Objem palivových nádrží: Fuel Tank Capacity: | 2540 l 3x 568 nebo 1041 l přídavná nádrž | 671 US gal 3x 150 or 275 gal drop tank |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | ~1604 km/h v 10093 m | ~997 mph in 36000 ft |
| Cestovní rychlost: Cruise Speed: | ~882 km/h v ? m | ~548 mph in ? ft |
| Rychlost stoupání: Climb Rate: | ~145 m/s | ~28536 ft/min |
| Čas výstupu na výšku: Time to Climb to: | ? min do ? m | ? min to ? ft |
| Operační dostup: Service Ceiling: | 15240+ m | 50000+ ft |
| Dolet: Range: | ~509 km | ~317 mi |
| Maximální dolet: Maximum Range: | 2861 km | 1778 mi |
| Výzbroj: Armament: | 2x kanon M39A2 ráže 20 mm, 280 nábojů každý 3175 kg výzbroje podvěšené na pěti nosnících 2x AIM-9 Sidewinder na koncích křídel | 2x M39A2 20-mm cannon, 280 rpg up to 7000 lb of ordnance on five pylons 2x AIM-9 Sidewinder at the wingtips |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | bývalé švýcarské F-5E pro agresorský výcvik u US Navy a US Marine Corps | ex-Swiss F-5E for aggressor training at US Navy and US Marine Corps |
| Zdroje: Sources: | Kinzey, Ben. F-5E & F Tiger II in detail & scale. Aero Publishers, Fallbrook 1982. ISBN 0-8168-5015-1. Johnsen, Frederick A. Northrop F-5/F-20/T-38. Specialty Press, North Branch 2006. ISBN 1-58007-094-9. http://joebaugher.com/usaf_fighters/f5_25.html www.navair.navy.mil www.navair.navy.mil www.navy.mil | |
Northrop F-5N Tiger II
F-5N Tiger II assigned to VFC-111 taking off from the airport Boca Chica Field on the NAS Key West, November 2014. The F-5N were introduced into the armament of units VFC-13 on NAS Fallon in Nevada, VFC-111 at NAS Key West Florida and VMFT-401 MCAS Yuma in Arizona..
(US Navy / Mass Communication Specialist 1st Class Brian Morales)
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(US Navy / Mass Communication Specialist 1st Class Brian Morales)
Reklama
F-5N Tiger II from the arsenal of the VFC-111 captured at the gate MCAS Beaufort in the framework of the joint exercise with the training unit of the maritime pechoty VMFAT-501, July 2016..
(USMC / SSgt Dengrier Baez)
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(USMC / SSgt Dengrier Baez)
F-5N Tiger II from the assembly VMFT-401 during the exercise, Marine Division Tactics Course to the MCAS Miramar, June 2017..
(USMC / Sgt Kimberlyn Adams)
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(USMC / Sgt Kimberlyn Adams)
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