Search filter

    • Year
      1906
      2018
    • Length
      15 m
      24 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      74 m2
      112 m2
    • Wingspan (Beam)
      25 m
      38 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      8
      13
    • 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
      5188 kg
      7784 kg
    • Max. takeoff weight (Gross weight)
      14515 kg
      21773 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      644 km/h
      966 km/h
    • Сruise Speed
      552 km/h
      828 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
      4633 l
      6951 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
      0 hp
      60000 hp
    • Thrust
      68 kN
      102 kN
    • Service ceiling
      17040 m
      25560 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      8246 km
      12370 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      9 h
      15 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
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 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
      83 qt
      125 qt
    • Price
      41 USD
      750000000 USD

Lockheed U-2

TypeAircraft
Company

Lockheed Corporation

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
19.2
88.7
Height (m)
0.6
 
4.9
50.1
Wings
Wing area (m2)
1.1
 
92.9
925
Wingspan (Beam) (m)
0.1
 
31.4
95
Aspect ratio
1.7
 
10.6
25.6
Weights
Empty weight (kg)
8
 
6,486
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
18,144
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
805
28,165
Сruise Speed (km/h)
52
 
690
3,087
Fuel
Fuel Capacity (l)
23
 
5,791.7
320,000
Power
Thrust (kN)
1.5
 
85
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
21,300
161,544
Range (Ferry range) (km)
4
 
10,308.2
40,700
Endurance (h)
0.0
 
12
150
Stat
Number built (qt)
0
 
104
43,000
Introduction 1955
First flight 01.08.1955

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