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Concorde - Celebrating twenty-seven supersonic years

Photograph showing detail of the engine exhausts of Tu-144d CCCP-77112
Photograph of the port wing and engine housings of Tupolev Tu-144d CCCP-77112

Tu-144 Specification

The following figures represent the specification for the Tupolev Tu-144 prototype aircraft and the two production-specification aircraft.

Length
58.5m/192ft 1
65.7m/215ft 2
67.5m/221ft 3
Height
12.85m/42ft 1, 2, 3
Wingspan
27m/88ft 1
28m/92ft 2
28.8m/94ft 3
Wing Area
469.8m2/5057ft2  1
503m2/5414ft2  2
506.9m2/5456ft2  3
Weight (empty)
79,000kg/174,000lbs 1
85,150kg/188,000lbs 2
86,900kg/192,000lbs 3
Engines
Kuznetsov NK-144 1
Kuznetsov NK-144F 2
Kuznetsov RD-36-51 3
Cruising speed
2430kph/1510mph (Mach 2.29) 1
2000kph/1240mph (Mach 1.88) 2
2124 kph/1319mph (Mach 2.0) 3
Cruising altitude
20,000m/65,000ft 1, 2
18,900m/62,000ft3
Flying range
2,500 km/2550 miles 1
3,080 km/1914 miles 2
6,500 km/4039 miles 3
Passengers
126 1
140 2
155 3
Crew
6 1
3 2, 3

[Note 1: Tupolev Tu144; 2: Tupolev Tu144s; 3: Tupolev Tu144d]

Richard Coltman 2007