Tupolev Tu-104

· Tupolev

Airplanes

Length

40.06 m

Flat Wing Span

34.54 m

Height

11.9 m

Flat Wing Area

183 m²

Max Seating

115

Max Speed

950 km/h

Max Ceiling

12000 m

Number of Engines

First Flight

1955-06-17

Entry Into service

1956-09-15

Number Built

201

Maximum Range

2120 km

Pictures

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Aircraft	Maximum Range (km)
Tupolev Tu-104	2120

Name	Family	Aircraft Engine	Length (m)	Flat Wing Span (m)	Two Class Typical Seating	Max Seating
Tupolev Tu-107			38.58	34.54		70	Compare
737-600		CFM International CFM56	39.47	35.79		160	Compare
Yakovlev Yak-46		Progress D-27	41	35.5			Compare
737-8	737 MAX	LEAP-1B28/28B1/28B2/28B3	39.52	35.92	178	189	Compare
Antonov An-180		Progress D-27	40.9	35.83			Compare
727-200		Pratt & Whitney JT8D	40.5384	32.9184		106	Compare

All data (25 fields)

Name: Tupolev Tu-104
Manufacturer: Tupolev
Description: The Tupolev Tu-104 (NATO reporting name: Camel) is a medium-range, narrow-body, twin turbojet-powered Soviet airliner.
First Flight: 1955-06-17
Entry Into service: 1956-09-15
Production End: 1960-01-01
Service End: 1981-01-01
Designer: Andrei Tupolev
Type: Narrow-body jetliner
Length (m): 40.06
Height (m): 11.9
Cockpit Crew: 7
Max Seating: 115
Max Speed (km/h): 950
Max Ceiling (m): 12000
Rate of Climb (m/s): 10
Capacity Description: 50–115 passengers
Number Built: 201
Powerplant Description: 2 × Mikulin AM-3M-500 turbojet engines
Primary Users: Aeroflot, ČSA
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Tupolev_Tu-104
Flat Wing Span (m): 34.54
Flat Wing Area (m²): 183
Number of Engines: 2