Shenyang J-8 | |
|---|---|
| 国 | 中国 |
| 役割 | インターセプター |
| 初飛行 | 1969年7月5日 |
| 構築 | 408 |
ザ 瀋陽 J-8 (中国語: 歼-8;NATO報告名:フィンバック)は、中華人民共和国(中国)の601研究所(瀋陽)によって開発された迎撃機です。
ソース： ウィキペディアの瀋陽J-8
| 瀋陽 J-8 | |
|---|---|
| カメラマン | 知りません |
| ローカライズ | 知りません |
| 写真 | 54 |
瀋陽J-8 01
瀋陽 J-8 02
瀋陽 J-8 03
瀋陽J-8 04
瀋陽 J-8 05
瀋陽J-8 06
瀋陽 J-8 07
瀋陽 J-8 08
瀋陽J-8 09
待って、瀋陽J-8を探しています...
関連項目:
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) |
|---|---|
| 役割 | High-Altitude Interceptor / All-Weather Fighter |
| メーカー | Shenyang Aircraft Corporation (SAC) |
| First Flight (Original J-8) | July 5, 1969 |
| 乗組員 | 1 pilot |
| 長さ | 21.59 m (70 ft 10 in) |
| 翼 | 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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