Tupolew Tu-134

Tupolew Tu-134
Kraju	Związek Radziecki – Rosja
Roli	Samolot
Pierwsza mucha	29 lipca 1963
Zbudowany	854

Tthe Tupolew Tu-134 (nazwa NATO: Crusty) to dwusilnikowy, wąskokadłubowy odrzutowy samolot pasażerski zbudowany w Związku Radzieckim do lotów krótko- i średniodystansowych w latach 1966 - 1989. Pierwotna wersja miała przeszklony nos i, podobnie jak niektóre inne rosyjskie samoloty pasażerskie (w tym siostrzany model Tu-154), mogła operować z nieutwardzonych lotnisk.

Źródła: Tupolew Tu-134 na Wikipedii

Tupolew Tu-134A Spacer
Fotograf	Władimir Yakubov
Lokalizacja	Muzeum Lotnictwa w Mińsku-Borowej, Białoruś
Zdjęcia	149

Tupolev Tu-134A 01

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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)
Roli	Short/Medium-Haul Airliner
Producent	Kharkov State Aircraft Plant / Tupolev Design Bureau
Entered Service (Tu-134A)	1970
Załogi	3 or 4 (Pilot, Co-pilot, Flight Engineer/Navigator)
Pojemność	72 to 84 passengers
Długość	37.10 m (121 ft 8 in)
Rozpiętość	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.

Liczba wyświetleń : 261