Tupolew / Tupolev Tu-104

Airliner

Tupolew / Tupolev Tu-104 © Alexander Marcenco
Photo ©: Alexander Marcenco (Photos at airliners.net)
The Tupolev Tu-104 is a twin-engined medium-range narrowbody jet airliner with a capacity of 100 passengers developed by the Soviet Design Bureau OKB Tupolev.
The Tu-104 is a civil development of the Tupolev Tu-16 bomber. The Tu-104 was the world's second jet airliner after the de Havilland D.H.106 Comet.
Crew5
Passengers70-100
Propulsion2 Turbojet Engines
Engine ModelMikulin AM-3M-500
Engine Power (each)93,1 kN20930 lbf
Speed950 km/h513 kts
  590 mph
Service Ceiling11.500 m37.730 ft
Range2.650 km1.431 NM
1.647 mi.
Empty Weight41.600 kg91.712 lbs
max. Takeoff Weight76.000 kg167.551 lbs
Wing Span34,54 m113 ft 4 in
Wing Area183,5 m1975 ft
Length40,05 m131 ft 5 in
Height11,90 m39 ft 1 in
First Flight17.06.1955
Production Statusout of production
Total Productionca. 200
Developed fromTupolew / Tupolev Tu-16
NATO CodeCamel
Data for (Version)Tupolev / Tupolew Tu-104B
VariantsTu-104A, Tu-104B

[Photo-ID: 10575] Karsten Palt 2014-06-08
Tupolev Tu-104A, CSA - Ceskoslovenske Aerolinie, OK-LDA, c/n 76600503, Karsten Palt, 2014Tupolev
Tu-104A
CSA - Ceskoslovenske Aerolinie
Reg.: OK-LDA
c/n: 76600503
 
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