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    • Year
      1906
      2018
    • Length
      24 m
      38 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      112 m2
      170 m2
    • Wingspan (Beam)
      13 m
      21 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
      19840 kg
      29760 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      880 kg
      1320 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      2848 km/h
      4272 km/h
    • Сruise Speed
      1700 km/h
      2550 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
      36944 l
      55416 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      230 kN
      346 kN
    • Service ceiling
      23200 m
      34800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3200 km
      4800 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
      28800 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
      9 qt
      15 qt
    • Price
      41 USD
      750000000 USD

Lockheed A-11

TypeAircraft
Company

Lockheed Corporation

Scheme

Integrated

Monoplane

Geometry
Length (m)
1.9
 
31.0
88.7
Height (m)
0.6
 
5.6
50.1
Wings
Wing area (m2)
1.1
 
141.1
925
Wingspan (Beam) (m)
0.1
 
17.0
95
Weights
Empty weight (kg)
8
 
24,800
276,800
Capacity
Crew (per.)
1
 
1
112
2 for trainer variant
Payload (kg)
23
 
1,100
122,470
of reconnaissance sensors
Speeds
Max. Speed (km/h)
25
 
3,560
28,165
at 23000
Сruise Speed (km/h)
52
 
2,125
3,087
Fuel
Fuel Capacity (l)
23
 
46,180
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.6
2.1
Thrust (kN)
1.5
 
288
1,914
2 powerplants 144 kN each
Performance
Service ceiling (m)
0.6
 
29,000
161,544
Range (Ferry range) (km)
4
 
4,000
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
36,000
36,000
Stat
Number built (qt)
0
 
12
43,000
Introduction 1962
First flight 26.04.1962
Stop production 1968

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