Aérospatiale-BAC Concorde [+]Compare [E]dit [H]istory

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Object «Aérospatiale-BAC Concorde» has attributes

Attribute Value
General
Manufacturer Aérospatiale
Model Aérospatiale-BAC Concorde
Country France
Manufactured from 1965 year
Manufactured to 1979 year
Type Mid Size Passenger Jets
Icao CONC
Performance
Engine 4x 4 × Rolls-Royce/SNECMA Olympus 593 Mk 610
Power, hp Add
Power, lbf 38,050 lbf
Avionics Fly by wire flight controls, Digital Air Intake Control Units
Max cruise speed 2,330 km/h
Approach speed 306 km/h
Travel range 7,223 km
Fuel economy 0.059 km/l
Service ceiling 18,288 m
Rate of climb 25.4 m/sec
Take off distance 3,429 m
Landing distance 2,200 m
Weights
Max take off weight 185,070 kg
Max landing weight Add
Max payload 11,000 kg
Fuel tank capacity 119,178 l
Baggage volume 6.71 m³
Dimensions
Seats 128
Seats - business class 12
Seats - first class 92
Cabin height 1.96 m
Cabin width 2.63 m
Cabin length 39.32 m
Exterior length 61.66 m
Tail height 12.2 m
Fuselage diameter 2.87 m
Wing span 25.6 m
Wing tips No Winglets

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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 25, 2021 (50 fields were changed)
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