Comparison of Lockheed L-1011 TriStar 200 and Tupolev Tu-16

Attribute	Lockheed L-1011 TriStar 200 ×	Tupolev Tu-16 ×
General
Manufacturer	Lockheed Martin Aeronautics	Tupolev
Model	Lockheed L-1011 TriStar 200	Tupolev Tu-16
Country	United States	Russia
Manufactured from (year)	1968	1953
Manufactured to (year)	1984	1962
Type	Jumbo Passenger Jets	Military Aircraft
Icao	L101	TU16
Performance
Engine	3x RB211-524B	2x Mikulin AM-3 M-500
Power, lbf (lbf)	50,000	21,000
Avionics	L-1011 Avionics Flight Control System	-
Max cruise speed (km/h)	954	1,056
Approach speed (km/h)	269	-
Travel range (km)	6,667	7,223
Service ceiling (m)	12,802	12,802
Rate of climb (m/sec)	14.22	12.7
Take off distance (m)	2,350	-
Landing distance (m)	1,960	-
Weights
Max take off weight (kg)	211,374	79,000
Max landing weight (kg)	166,922	76,000
Max payload (kg)	33,656	9,000
Fuel tank capacity (l)	100,321	42,396
Baggage volume (m³)	97.2	-
Dimensions
Seats	4	7
Cabin height (m)	2.7	-
Cabin width (m)	5.77	-
Cabin length (m)	33	-
Exterior length (m)	54.17	34.8
Tail height (m)	16.87	10.36
Fuselage diameter (m)	5.97	2.5
Wing span (m)	47.35	33
Wing tips	No Winglets	No Winglets