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/ Comparison of Hawker Siddeley HS-121 Trident and de Havilland DH-106 Comet 4
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Comparison of Hawker Siddeley HS-121 Trident and de Havilland DH-106 Comet 4
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Attribute
Hawker Siddeley HS-121 Trident
×
de Havilland DH-106 Comet 4
×
General
Manufacturer
Hawker Beechcraft
de Havilland
Model
Hawker Siddeley HS-121 Trident
de Havilland DH-106 Comet 4
Country
United States
United Kingdom
Manufactured from (year)
1964
1952
Manufactured to (year)
1978
1964
Type
Mid Size Passenger Jets
Mid Size Passenger Jets
Icao
TRID
-
Performance
Engine
3x 3 × Rolls-Royce RB.163-25 Spey 512
4x 4 × Rolls-Royce Avon Mk 524 turbojets
Power, lbf (lbf)
11,960
10,500
Max cruise speed (km/h)
972
900
Travel range (km)
3,860
5,189
Fuel economy (km/l)
0.21
0.152
Service ceiling (m)
10,668
12,802
Rate of climb (m/sec)
15.24
-
Take off distance (m)
840
2,290
Landing distance (m)
675
-
Weights
Max take off weight (kg)
68,000
73,483
Max payload (kg)
14,692
10,930
Fuel tank capacity (l)
24,730
39,520
Dimensions
Seats
18
81
Seats - business class
115
81
Seats - first class
-
56
Cabin height (m)
2
-
Cabin width (m)
3.4
-
Cabin length (m)
9.14
-
Exterior length (m)
40
34
Tail height (m)
8.6
8.99
Fuselage diameter (m)
3.6
-
Wing span (m)
29.9
35
Wing tips
No Winglets
No Winglets
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