Tupolev Tu-144S

Public Joint Stock Company Tupolev

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Tupolev Tu-144S aircraft
Public Joint Stock Company TupolevTupolev Tu-144

Photograph of the Tupolev Tu-144 family. No photograph on Wikimedia Commons identifies this variant specifically.

Photo: Ank Kumar · CC BY-SA 4.0 · Modified

About

The Tupolev Tu-144S is the standard production variant of the Tu-144 supersonic transport, representing the operational configuration delivered to Aeroflot for commercial service from 1977 to 1978. Built upon lessons learned from the prototype and early test aircraft, the Tu-144S features refined systems, improved structural integrity, and operational enhancements for airline service. Powered by four Kuznetsov NK-144A afterburning turbofan engines producing enhanced thrust and reliability compared to the prototype NK-144 engines, the Tu-144S maintains the distinctive delta wing with retractable canard foreplanes that deploy for takeoff and landing, providing crucial low-speed lift and control. The aircraft features a cruise speed of Mach 2.07 (2,200 km/h) at altitude, which was slightly reduced from the maximum design speed to improve fuel efficiency and reduce structural stress during regular operations. The Tu-144S accommodates 98-120 passengers depending on cabin configuration, with early commercial service using a 98-seat two-class layout (11 first class at 4-abreast, 87 economy at 5-abreast seating) to provide premium service on prestige international routes. The practical range of approximately 3,080 kilometers (1,914 miles) with full passenger load limited operations primarily to domestic Soviet routes, with the Moscow-Almaty route becoming the primary commercial service between November 1977 and June 1978. The Tu-144S retained the droop nose for pilot visibility during approach and landing, a design feature shared with Concorde. Despite operational challenges including high fuel consumption (approximately 3 times higher than subsonic jets per passenger-kilometer), excessive cabin noise levels approaching 90-95 dB during supersonic cruise (making conversation extremely difficult), and limited route network due to range constraints and sonic boom restrictions, the Tu-144S represented the pinnacle of Soviet supersonic transport technology. Commercial passenger service ended after only 55 scheduled flights due to economic and operational challenges, though cargo operations continued into the early 1980s.

Weightscompared to Boeing 757-300

MTOW (Maximum Takeoff Weight)

180,000kg
0
100k
180k

MLW (Maximum Landing Weight)

150,000kg
0
50k
100k
150k

Empty Weight

85,000kg
0
50k
100k

Capacitycompared to Boeing 757-300

Passenger Capacity

120passengers
0
100
200
295

41% of 757-300 maximum capacity

Crew

Total
7
Cockpit
3
Cabin
4

Dimensions

Length

65.7m

Wingspan

28.8m

Height

10.5m

Wing Area

438.0m²

Cabin Width

3.45m

Engine Specifications

Engine Count

4×

Engine Model

Kuznetsov NK-144A

Thrust per Engine

196.1 kN(44094 lbf)

Fuel & Cargo

Fuel Capacity

87,500 L

Cargo Volume

20 m³

Production & History

Production Status

Out of production

Manufacturing Period

1973–1983

First Flight

January 1, 1973

Entered Service

November 1, 1977

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