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    • Year
      1906
      2018
    • Length
      28 m
      43 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      137 m2
      207 m2
    • Wingspan (Beam)
      36 m
      55 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      1
      26
    • Disc area
      1 m2
      460 m2
    • Main rotor diameter
      1 m
      62 m
    • Rotor number
      1 qt
      8 qt
    • Blades per rotor
      4 qt
      5 qt
    • Disc loading
      17 kg/m2
      73 kg/m2
    • Tail rotor diameter
      0 m
      5 m
    • Empty weight
      36455 kg
      54683 kg
    • Max. takeoff weight (Gross weight)
      56646 kg
      84970 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      6 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      79 per.
      119 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      485 km/h
      729 km/h
    • Сruise Speed
      373 km/h
      561 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      107 km/h
      1050 km/h
    • Fuel Capacity
      29811 l
      44717 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      10880 hp
      16320 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5780 m
      8670 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      6360 km
      9540 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      3 qt
      5 qt
    • Prop diameter
      4 m
      6 m
    • Prop blade number
      2 qt
      4 qt
    • Guns
      1 qt
      18 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      35 qt
      53 qt
    • Price
      2400000 USD
      3600000 USD

Lockheed L-1649 Starliner

TypeAircraft
Company

Lockheed Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
35.1
88.7
Height (m)
0.6
 
7.5
50.1
Wings
Wing area (m2)
1.1
 
171.9
925
Wingspan (Beam) (m)
0.1
 
45.7
95
Weights
Empty weight (kg)
8
 
45,569
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
70,807.6
575,000
Capacity
Crew (per.)
1
 
5
112
Capacity passengers (per.)
1
 
99
400
Speeds
Max. Speed (km/h)
25
 
607
28,165
Сruise Speed (km/h)
52
 
467
3,087
Fuel
Fuel Capacity (l)
23
 
37,264
320,000
Power
Total Power (hp)
0.4
 
13,600
60,000
4 powerplants 3400 hp each
Performance
Service ceiling (m)
0.6
 
7,225
161,544
Range (Ferry range) (km)
4
 
7,950
40,700
7950-9945 km
Propellers
Propellers (qt)
1
 
4
8
1 per engine
Prop diameter (m)
1.8
 
5.8
5.8
Prop blade number (qt)
1
 
3
8
3 per engine
Stat
Number built (qt)
0
 
44
43,000
Price (USD)
41.5
 
3.0 million
750.0 million
Introduction 01.06.1957
First flight 10.10.1956
Stop production 1980

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