Tupoljev Tu-134

Tupoljev Tu-134
Zemlja	Sovjetski Savez – Rusija
Ulogu	Putnički avion
Prva muva	29. jul 1963.
Izgradio	854

Čaj Tupoljev Tu-134 (NATO izveštavanje ime: Crusti) je dvomotorni, uskog tela mlazni putnički avion izgrađen u Sovjetskom Savezu za kratke i srednje rute od 1966 do 1989. Originalna verzija je imala dizajn zastakljenog nosa i, kao i neke druge ruske aviokompanije (uključujući i njegov sestrinski model Tu-154), može da radi sa neasfaltiranih aerodroma.

Izvor: Tupoljev Tu-134 na Vikipediji

Tupoljev Tu-134A Walk Around
Fotograf	Vladimir Jakubov
Lokalizacija	Vazdušni muzej Minsk-Borovaja, Belorusija
Fotografije	149

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Tupolev Tu-134A 09

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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)
Ulogu	Short/Medium-Haul Airliner
Proizvođača	Kharkov State Aircraft Plant / Tupolev Design Bureau
Entered Service (Tu-134A)	1970
Posada	3 or 4 (Pilot, Co-pilot, Flight Engineer/Navigator)
Kapacitet	72 to 84 passengers
Dužina	37.10 m (121 ft 8 in)
Raspon krila	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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