ツポレフTu-134 | |
|---|---|
| 国 | ソビエト連邦 – ロシア |
| 役割 | 旅客機 |
| ファーストフライ | 1963年7月29日 |
| 構築 | 854 |
ザ ツポレフTu-134 (NATO報告名:クラスティ)は、1966年から1989年までソビエト連邦で短距離および中距離路線向けに製造された双発のナローボディジェット旅客機です。オリジナル版は艶出しの機首のデザインが特徴で、他のロシアの旅客機(姉妹モデルのTu-154を含む)と同様に、未舗装の飛行場から運用できる。
ソース： ウィキペディアのツポレフTu-134
| ツポレフTu-134A歩 | |
|---|---|
| カメラマン | ウラジーミル・ヤクボフ |
| ローカライズ | ミンスク・ボロバヤ航空博物館(ベラルーシ) |
| 写真 | 149 |
Tupolev Tu-134A 01
Tupolev Tu-134A 02
Tupolev Tu-134A 03
Tupolev Tu-134A 04
Tupolev Tu-134A 05
Tupolev Tu-134A 06
Tupolev Tu-134A 08
Tupolev Tu-134A 07
Tupolev Tu-134A 09
待って、検索ツポレフTu-142のために.
関連項目:
General Characteristics (Soviet Era)
The Tupolev Tu-134 is a twin-engine, short-to-medium-range jet airliner developed in the Soviet Union, originally conceived to replace the Ilyushin Il-14. The ‘A’ variant was the first major production modification, introducing improved engines and increased passenger capacity.
| Property | Value (Tu-134A Variant) |
|---|---|
| 役割 | Short/Medium-Haul Airliner |
| メーカー | Kharkov State Aircraft Plant / Tupolev Design Bureau |
| Entered Service (Tu-134A) | 1970 |
| 乗組員 | 3 or 4 (Pilot, Co-pilot, Flight Engineer/Navigator) |
| 能力 | 72 to 84 passengers |
| 長さ | 37.10 m (121 ft 8 in) |
| 翼 | 29.0 m (95 ft 2 in) |
Design and Powerplant
- Engines: Two Soloviev D-30-II or D-30-III turbofan engines.
- Engine Placement: A distinctive feature, the engines are mounted in two nacelles on the sides of the rear fuselage (similar to the BAC One-Eleven or Douglas DC-9).
- Thrust (D-30-II): Approx. 66.7 kN (15,000 lbf) per engine.
- Cockpit: Features a glazed nose, originally intended for a navigator, a hallmark of early Soviet jet transport design (though sometimes phased out on later A models).
- Wing Design: Features a swept wing with noticeable dihedral and leading-edge slats for improved low-speed handling.
- Landing Gear: Equipped with low-pressure tires for operation from unprepared airfields, a common Soviet design requirement.
Performance and Variants
- Maximum Cruise Speed: 900 km/h (560 mph, 486 knots).
- Operational Range: Approximately 1,800 to 2,000 km (1,100 to 1,240 miles).
- Service Ceiling: 12,100 m (39,700 ft).
- Key Improvement (Tu-134A): Compared to the original Tu-134, the ‘A’ variant has a stretched fuselage for more seating and an improved turbofan engine. It also replaced the rear braking parachute with reverse thrust on the engines.
- Noise Issues: Due to the high exhaust velocity of its early turbofan engines, the Tu-134 family was known to be extremely loud and was one of the first Soviet types to be banned from many European airports due to noise restrictions in the 1990s and 2000s.
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