심양 J-8

Shenyang J-8

국가중국
역할인터셉터
첫 비행1969년 7월 5일
내장408

Tthe 심양 J-8 (중국어: 歼-8; NATO 보고명: Finback)은 중화인민공화국(중국) 601 연구소(선양)에서 개발한 요격기이다.

소스: 선양 J-8 ― 위키피디아

심양 J-8
사진 작가Unknow
로컬라이제이션Unknow
사진54
대기,검색 심양 J-8 당신을 위해...

Military Fighter Alloy Die Cast Model, 1/72 Scale Shenyang J-8 Finback Fighter Model, Adult Toys and Decorations, 11.7 x 5.1Inch - Amazon

참고 항목:

World War II: The Definitive Visual History from Blitzkrieg to the Atom Bomb(DK Definitive Visual Histories) - 아마존 지도별 제2차 세계 대전 지도(DK History Map by Map) - 아마존


General Characteristics (J-8II/Finback-B Variant)

The Shenyang J-8, code-named Finback by NATO, is a Chinese twin-engine, single-seat interceptor fighter. The original J-8 design, with a nose intake (Finback-A), was an enlarged, twin-engine derivative of the MiG-21/J-7. The significantly redesigned J-8II replaced the nose cone with a solid radome and side intakes to accommodate a larger fire-control radar, turning it into a more capable all-weather fighter.

Property Typical Value (J-8II)
역할 High-Altitude Interceptor / All-Weather Fighter
제조업체 Shenyang Aircraft Corporation (SAC)
First Flight (Original J-8) July 5, 1969
승무원 1 pilot
길이 21.59 m (70 ft 10 in)
윙스 팬 9.34 m (30 ft 8 in)
Max Takeoff Weight 17,800 kg (39,242 lb)

Design and Powerplant

  • Engines: Two Liyang Wopen-13A-II afterburning turbojets (on J-8II).
  • Thrust Output (with afterburner): Approximately 65.9 kN (14,815 lbf) each.
  • Design Origin: The early J-8 was heavily influenced by the Soviet MiG-21, specifically featuring a delta wing and conventional tail.
  • J-8II Redesign: The J-8II adopted a new forward fuselage with side air intakes (similar to the MiG-23) to allow the nose to house a more powerful pulse-Doppler radar.
  • Construction: Predominantly all-metal construction.
  • Variants: Later variants (J-8D, J-8F, J-8H) added features like in-flight refueling (IFR) probes, upgraded avionics, and improved weapon compatibility.

Performance and Armament

  • Maximum Speed: Mach 2.2 (around 2,340 km/h or 1,453 mph) at high altitude.
  • Service Ceiling: 20,200 m (66,275 ft).
  • Maximum Range (Ferry): Approximately 2,200 km (1,400 nautical miles) with external tanks.
  • Rate of Climb: High rate, approximately 12,000 m/min (39,370 ft/min).
  • Fixed Armament (J-8II): One 23 mm Type 23-3 (GSh-23L) twin-barrel cannon.
  • Hardpoints: Typically seven external hardpoints (one centerline, six underwing).
  • Typical Armament Options: PL-2/PL-5/PL-7 short-range IR-homing air-to-air missiles; later variants (J-8D/F) integrated medium-range radar-guided missiles like the PL-11 or PL-12.

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