TUPOLEV TU-144 Civil Aircraft Model Details

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General Information of TUPOLEV TU-144

First Flight : 31 December 1968[1]

Introduction : 1 November 1977[1]

Manufacturer : Tupolev OKB

Number Built : 16

Primary Users : Aeroflot; Ministry of Aviation Industry (Soviet Union); NASA

Produced : 1963–1983

Role : Supersonic airliner

Status : Retired

General characteristics of TUPOLEV TU-144

Capacity : 140 passengers (11 1-st class & 129 tourist class)

Crew : 3

Empty Weight : 99,200 kg (218,500 lb)

Height : 12.50 m (41.00 ft)

Length : 65.50 m (215.54 ft)

Loaded_Weight : 125,000 kg (275,330 lb)

Max Takeoff Weight : 207,000 kg (455,950 lb)

Powerplant : 4 × Kolesov RD-36-51 turbojet, 200 kN (44,122 lbf)[N 6] each

Wing Area : 506.35 m² (5,450 ft²)

Wingspan : 28.80 m (94.48 ft)

Performance of TUPOLEV TU-144

Cruise Speed : Mach 2.15 (2,120km/h (1,320mph))

Rate Of Climb : 3,000 m/min (9,840 ft/min)

Service Ceiling : 20,000 m (65,600 ft)

Wing Loading : 410.96kg/m² (84.20 lb/ft²)

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