Tupolev Tu-114 technical information

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777
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Tupolev Tu-114 technical information

Post by 777 »

Tupolev Tu-114 Roosiya NATO codename: Cleat

Long-Range Jetliner



DESCRIPTION:
Just as Tupolev had successfully adapted the Tu-16 bomber into the Tupolev Tu-104 medium-range airliner, the design bureau was instructed to develop an airliner with intercontinetal range based on the Tu-95. The resulting Tu-114, like its military cousin, came as a great surprise to western observers shocked that a propeller-driven aircraft could operate at jet-like speeds. The key to the success of the Tu-95/Tu-114 family was the development of the enormous and powerful NK-12 turboprop designed by the Kuznetsov Design Bureau, although most of the work was done by a team of captured German scientists. Still the most powerful turboprop engine ever built, the NK-12 converted its shaft power into thrust through gigantic four-bladed counter-rotating propellers mounted in pairs on each engine. While the Tu-114 was still being designed, the bureau decided to quickly build three demilitarized Tu-95s, known as the Tu-116, to conduct route and scheduling studies, propulsion system tests, and study compatability issues with civil airports. Common to the Tu-95, Tu-116, and Tu-114 were the four engines, enormous swept wing, and long landing gear units necessitated by the large-diameter propellers. But while the Tu-116 prototypes utilized essentially the same fuselage as the Tu-95, the Tu-114 incorporated a completely new fuselage of increased diameter permitting greater internal volume. In addition, the wing was mounted lower on the fuselage improving the passenger cabin floor layout. The flight crew was seated in a nose reminsicent of that on the Tu-95 bomber including a a glazed window encasing the navigator's position in the extreme nose. The main cabin was huge by 1950's standards with accomodation for 120 to 220 passengers. The forward cabin seating 42 was followed by a section of large coat closets, a dining compartment seating 48, a galley with elevators bringing up food from the kitchen on the lower deck, a small compartment seating two of the five cabin crew, two small compartments providing additional seating or sleeping berths, the main cabin seating 54, and washrooms. After setting a number of records, including a speed record for fastest turboprop-powered aircraft that still stands today, the first of 31 Tu-114s entered service with Aeroflot. In addition to long-range domestic routes, the Tu-114 also served Delhi, Havana, Montreal, Paris, and Copenhagen as well as Tokyo in flights operated jointly with Japan Air Lines and flown by mixed Soviet-Japanese crews. The Tu-114 began to be replaced by the Il-62 in 1971 and was withdrawn from civil service in 1975, but several were given a new lease on life after being converted into Tu-126 airborne early warning platforms.
Last modified 4 February 2002



HISTORY:
First Flight (Tu-116) late 1956
(Tu-114) 3 October 1957
Service Entry

24 April 1961


CREW: 5 flight crew: 1 pilot, 1 co-pilot, 1 navigator, 1 radio operator, 1 flight engineer
5 cabin crew: 3 flight attendants, 2 cooks


PASSENGERS: 120 long-range nonstop flights
170 normal operations
220 high-density


ESTIMATED COST:

unknown


AIRFOIL SECTIONS:
Wing Root TsAGI SR-5S
Wing Tip

TsAGI SR-5S


DIMENSIONS:
Length 177.33 ft (54.10 m)
Wingspan 167.50 ft (51.10 m)
Height 50.67 ft (15.50 m)
Wing Area 3,348.76 ft2 (311.10 m2)
Canard Area

not applicable


WEIGHTS:
Empty 200,620 lb (91,000 kg)
Typical Load unknown
Max Takeoff 376,990 lb (171,000 kg)
Fuel Capacity internal: 18,920 gal (71,615 L)
external: not applicable
Max Payload

66,140 lb (30,000 kg)


PROPULSION:
Powerplant four Kuznetsov NK-12MV turborpops each driving two AV-60H counter-rotating four-balded reverse-pitch propellers
Thrust 59,180 eshp (44,132 ekW)


PERFORMANCE:
Max Level Speed at altitude: 540 mph (870 km/h) at 26,250 ft (8,000 m), Mach 0.78
at sea level: unknown
cruise speed: 480 mph (770 km/h) at 29,500 ft (9,000 m), Mach 0.70
Initial Climb Rate unknown
Service Ceiling 39,370 ft (12,000 m)
Range 4,830 nm (8,950 km) with 33,070 lb (15,000 kg) payload
3,345 nm (6,200 km) with 66,140 lb (30,000 kg) payload
Endurance unknown
g-Limits unknown


KNOWN VARIANTS:
Tu-116 Demilitarized Tu-95 bomber used as a prototype with the weapons bay and tail turret deleted and a 24 or 30 seat four-abreast pressurized passenger cabin added to the aft fuselage; 1 modified and 2 built
Tu-114 Production long-range jetliner; 31 built
Tu-114D Aeroflot designation applied to the three Tu-116 aircraft
Tu-126 Designation applied to former Tu-114 airframes withdrawn from service and converted into airborne early warning and control (AWACS) platforms for the Soviet Navy


KNOWN OPERATORS: Aeroflot
Japan Air Lines


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Andre

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liebensd
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Post by liebensd »

André,

Can't you better make on toppic about technical info and post every aircraft in it?


Greetz,

Dave

329
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Joined: 26 Oct 2003, 00:00
Location: Antwerp

Post by 329 »

Hi 777, it is intresting to see the difference

between the TU-114 and TU-144 which is often

confusing.

Now it is clear


John

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Comet
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Post by Comet »

I wouldn't have thought there was any confusion between a Tu114 and a Tu144 - one is a prop, the other is a supersonic transport.

Not much difference there!!!
Sabena and Sobelair - gone but never forgotten.
Louise

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