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/ Comparison of Hawker Siddeley HS-121 Trident and Lockheed L-1011 TriStar 500
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Comparison of Hawker Siddeley HS-121 Trident and Lockheed L-1011 TriStar 500
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Attribute
Lockheed L-1011 TriStar 500
×
Hawker Siddeley HS-121 Trident
×
General
Manufacturer
Lockheed Martin Aeronautics
Hawker Beechcraft
Model
Lockheed L-1011 TriStar 500
Hawker Siddeley HS-121 Trident
Country
United States
United States
Manufactured from (year)
1968
1964
Manufactured to (year)
1984
1978
Type
Mid Size Passenger Jets
Mid Size Passenger Jets
Icao
L101
TRID
Performance
Engine
3x 3 x Rolls-Royce RB.211-524B
3x 3 × Rolls-Royce RB.163-25 Spey 512
Power, lbf (lbf)
50,000
11,960
Max cruise speed (km/h)
972
972
Travel range (km)
9,906
3,860
Fuel economy (km/l)
0.059
0.21
Service ceiling (m)
13,106
10,668
Rate of climb (m/sec)
14.33
15.24
Take off distance (m)
2,426
840
Landing distance (m)
1,734
675
Weights
Max take off weight (kg)
231,332
68,000
Max payload (kg)
42,003
14,692
Fuel tank capacity (l)
119,778
24,730
Baggage volume (m³)
420
-
Dimensions
Seats
246
18
Seats - business class
253
115
Seats - first class
234
-
Cabin height (m)
2.4
2
Cabin width (m)
5.8
3.4
Cabin length (m)
41.4
9.14
Exterior length (m)
50.05
40
Tail height (m)
16.8
8.6
Fuselage diameter (m)
6
3.6
Wing span (m)
50.1
29.9
Wing tips
No Winglets
No Winglets
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