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    • Year
      1906
      2018
    • Length
      19 m
      29 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
      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
      15748 kg
      23624 kg
    • Max. takeoff weight (Gross weight)
      29755 kg
      44634 kg
    • Loaded weight
      5 kg
      242500 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
      410 km/h
      616 km/h
    • Сruise Speed
      276 km/h
      416 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
      5600 hp
      8400 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7437 m
      11156 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3771 km
      5657 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
      195 m/min
      293 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
      2 qt
      4 qt
    • Bombs
      1 qt
      2 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      5120 kg
      7680 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      499 qt
      749 qt
    • Price
      41 USD
      750000000 USD

Avro Lincoln

TypeAircraft
Company

Avro Aircraft

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
23.9
88.7
Height (m)
0.6
 
5.3
50.1
Wings
Wing area (m2)
1.1
 
132.2
925
Wingspan (Beam) (m)
0.1
 
36.6
95
Weights
Empty weight (kg)
8
 
19,685.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
37,194.6
575,000
Capacity
Crew (per.)
1
 
7
112
pilot, flight engineer/co-pilot, navigator, wireless operator, front gunner/bomb aimer, dorsal and rear gunners
Speeds
Max. Speed (km/h)
25
 
513
28,165
at 5730 m
Сruise Speed (km/h)
52
 
346
3,087
at 6096 m
Power
Total Power (hp)
0.4
 
7,000
60,000
4 powerplants 1750 hp each
Performance
Service ceiling (m)
0.6
 
9,296.4
161,544
Range (Ferry range) (km)
4
 
4,714
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
243.8
36,000
Combat
Guns (qt)
1
 
3
18
2 × .50 in (12.7 mm) M2 Browning machine guns in nose and tail turrets, and dorsal turret with either twin .50 in machine guns or twin 20 mm Hispano cannon
Bombs (qt)
1
 
1
250
10,000 kg DP bomb (exceptionally)
Bombs weight (kg)
2
 
6,400
39,000
normal maximum
Stat
Number built (qt)
0
 
624
43,000
Introduction 1944
First flight 09.06.1944
Stop production 1967

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