
Pohjois-Amerikan FJ-4 Fury Tekniset tiedot
| Valmistaja | Pohjois-Amerikan ilmailu |
| Rooli | Lentotukialukseen perustuva hävittäjäpommittaja |
| Ensimmäinen lento | 3. lokakuuta 1954 |
| Johdanto | 1955 |
| Eläkkeellä | 1965 (Yhdysvaltain laivasto), 1972 (Venezuela) |
| Ensisijaiset käyttäjät | Yhdysvaltain laivasto, Venezuelan ilmavoimat |
| Luotu numero | 374 |
| Yksikkökustannus | 780 000 dollaria (FJ-4B) |
| Moottori | Yksi Pratt &; Whitney J48-P-8A -turbosuihkukone, työntövoima 7,250 lbf (32.3 kN) |
| Enimmäisnopeus | 680 mph (1 094 km/h) |
| Etäisyys | 1 200 mailia (1 900 km) |
| Huoltokatto | 44 000 jalkaa (13 400 m) |
| Aseistus |
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Nniiden Pohjois-Amerikan FJ-4 Fury oli pyyhkäisysiipinen lentotukialuskykyinen hävittäjäpommittaja Yhdysvaltain laivastolle ja merijalkaväelle. Viimeinen kehitys linjassa, johon kuului ilmavoimien F-86 Sabre, FJ-4 jakoi yleisen ulkoasunsa ja moottorinsa aikaisemman FJ-3: n kanssa, mutta siinä oli täysin uusi siipimuotoilu ja se oli huomattavasti erilainen muotoilu lopullisessa ruumiillistumassaan.
| North American FJ-4 Fury Walk Around | |
|---|---|
| Valokuvaaja | Vladimir Jakubov |
| Lokalisointi | Kansallinen ilma- ja avaruusmuseo |
| Valokuvat | 61 |
| North American FJ-4B ‘Fury’ Walk Around | |
|---|---|
| Valokuvaaja | Fotios Rouch |
| Lokalisointi | Ei tietää |
| Valokuvat | 58 |
Katso myös:
The Peak of the FJ Evolution
Nniiden Pohjois-Amerikan FJ-4 Fury was the final and most capable iteration of the Fury series. While it shared a common ancestry with the F-86 Sabre, by the time the FJ-4 arrived, it was a completely different beast. Designed primarily for the U.S. Marine Corps as a long-range, high-speed attack aircraft, it featured a deeper fuselage for increased fuel, a completely redesigned wing, and significantly improved landing gear. It transitioned the Fury from a pure dogfighter into a versatile strike platform capable of carrying nuclear weapons.
| Attribute | Technical Specification (FJ-4B) |
|---|---|
| Rooli | Carrier-based Fighter-Bomber / Strike Fighter |
| miehistö | 1 (Pilot) |
| First Flight | October 28, 1954 |
| Voimalaitos | 1 × Wright J65-W-16A turbojet |
| Thrust | 7,700 lbf (34 kN) |
| Enimmäisnopeus | 680 mph (1,094 km/h) at sea level |
| Aseistus | 4 × 20mm Colt Mk 12 cannons; 5 hardpoints (up to 6,000 lbs) |
| Missiles | AIM-9 Sidewinder (Fighter); AGM-12 Bullpup (Attack) |
Redesigned for the Strike Mission
- The “Deep” Fuselage: To address the short range of earlier jets, the FJ-4’s fuselage was noticeably “taller” or deeper than the FJ-1 or the F-86. This allowed it to carry 50% more internal fuel, giving it the “legs” needed for long-range interdiction.
- Thinner, Cleaner Wings: The FJ-4 featured a new, thinner wing with a different airfoil shape and a “cuffed” leading edge. This improved low-speed handling for carrier approaches while reducing drag at high subsonic speeds.
- All-Moving Tail: Like the F-86F, the FJ-4 used an “all-flying” tail (stabilator) which provided much better control authority when maneuvering near the speed of sound.
- FJ-4B Ground Attack: The “B” variant introduced an automated flight control system and a low-altitude bombing system (LABS) specifically designed for the delivery of tactical nuclear weapons.
Operational History and the Marine Corps
- The Marine’s Choice: While the Navy moved toward the F8U Crusader for air superiority, the Marine Corps leaned heavily on the FJ-4 for close air support. Its rugged design and heavy payload made it ideal for supporting troops from the deck of a carrier.
- Bullpup Pioneer: The FJ-4B was the first aircraft to carry the AGM-12 Bullpup, the world’s first mass-produced guided air-to-ground missile.
- Mid-Air Refueling: To further extend its range, the FJ-4 was equipped with a fixed refueling probe on the left wing, a standard feature for Naval aircraft of that era.
- Preservation: Because the FJ-4 was built in significant numbers (over 370), several are preserved in the US, including examples at the National Museum of the Marine Corps ja Maaliskuun kenttäilmamuseo.
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