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    • Year
      1906
      2018
    • Length
      21 m
      32 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      105 m2
      159 m2
    • Wingspan (Beam)
      29 m
      44 m
    • Wing loading
      240 kg/m2
      360 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
      18651 kg
      27978 kg
    • Max. takeoff weight (Gross weight)
      31207 kg
      46811 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      8 per.
      12 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
      384 km/h
      576 km/h
    • Сruise Speed
      52 km/h
      3087 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
      23 l
      320000 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
      6272 hp
      9408 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4925 m
      7389 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2889 km
      4334 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      3928 km
      5894 km
    • Endurance
      11 h
      18 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
      6 qt
      8 qt
    • Prop diameter
      3 m
      5 m
    • Prop blade number
      2 qt
      4 qt
    • Guns
      1 qt
      3 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      3628 kg
      5444 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      148 qt
      222 qt
    • Price
      41 USD
      750000000 USD

Avro Shackleton

TypeAircraft
Company

Avro Aircraft

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
26.6
88.7
Height (m)
0.6
 
5.3
50.1
Wings
Wing area (m2)
1.1
 
132.0
925
Wingspan (Beam) (m)
0.1
 
36.6
95
Wing loading (kg/m2)
3.1
 
300
829
Weights
Empty weight (kg)
8
 
23,314.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
39,008.9
575,000
Capacity
Crew (per.)
1
 
10
112
Speeds
Max. Speed (km/h)
25
 
480
28,165
Power
Total Power (hp)
0.4
 
7,840
60,000
4 powerplants 1960 hp each
Performance
Service ceiling (m)
0.6
 
6,157.0
161,544
Range (Ferry range) (km)
4
 
3,611.4
40,700
Сombat radius (km)
277
 
4,911
7,210
Endurance (h)
0.0
 
14.6
150
Propellers
Propellers (qt)
1
 
8
8
2 contra-rotating propellers per engine
Prop diameter (m)
1.8
 
4
5.8
Prop blade number (qt)
1
 
3
8
Combat
Guns (qt)
1
 
2
18
20 mm Hispano Mark V cannon in the nose
Bombs weight (kg)
2
 
4,536
39,000
of bombs, torpedoes, mines, or conventional or nuclear depth charges
Stat
Number built (qt)
0
 
185
43,000
Introduction 1949
First flight 09.03.1949
Stop production 1991

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