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    • Year
      1906
      2018
    • Length
      16 m
      26 m
    • Height
      5 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      96 m2
      145 m2
    • Wingspan (Beam)
      24 m
      38 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
      13229 kg
      19844 kg
    • Max. takeoff weight (Gross weight)
      26126 kg
      39191 kg
    • Loaded weight
      24727 kg
      37091 kg
    • Crew
      5 per.
      9 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
      363 km/h
      545 km/h
    • Сruise Speed
      280 km/h
      420 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
      4096 hp
      6144 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5218 m
      7828 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3258 km
      4888 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
      175 m/min
      264 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
      6 qt
      10 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      5080 kg
      7620 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      5901 qt
      8853 qt
    • Price
      62320 USD
      93480 USD

Avro Lancaster

TypeAircraft
Company

Avro Aircraft

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
21.1
88.7
Height (m)
0.6
 
6.3
50.1
Wings
Wing area (m2)
1.1
 
120.8
925
Wingspan (Beam) (m)
0.1
 
31.1
95
Weights
Empty weight (kg)
8
 
16,536.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
32,658.7
575,000
Loaded weight (kg)
5
 
30,909
242,500
Capacity
Crew (per.)
1
 
7
112
pilot, flight engineer, navigator, bomb aimer/nose gunner, wireless operator, mid-upper and rear gunners
Speeds
Max. Speed (km/h)
25
 
454
28,165
at 29000 kg and 4000 m
Сruise Speed (km/h)
52
 
350
3,087
Power
Total Power (hp)
0.4
 
5,120
60,000
4 powerplants 1280 hp each
Performance
Service ceiling (m)
0.6
 
6,522.7
161,544
at 29000 kg
Range (Ferry range) (km)
4
 
4,073
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
219.5
36,000
at 29000 kg and 2800 m altitude
Combat
Guns (qt)
1
 
8
18
2 Browning .303 Mark II machine guns in nose turret, 2 Browning .303 Mark II machine guns in upper turret, and 4 Browning .303 Mark II machine guns in the rear turret
Bombs weight (kg)
2
 
6,350
39,000
Stat
Number built (qt)
0
 
7,377
43,000
Price (USD)
41.5
 
77,900
750.0 million
Introduction 1941
First flight 09.01.1941
Stop production 1963

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