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    • Year
      1906
      2018
    • Length
      15 m
      23 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      86 m2
      130 m2
    • Wingspan (Beam)
      21 m
      32 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
      4782 kg
      7174 kg
    • Max. takeoff weight (Gross weight)
      6560 kg
      9840 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 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
      208 km/h
      312 km/h
    • Сruise Speed
      180 km/h
      270 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
      1236 l
      1854 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
      1040 hp
      1560 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3280 m
      4920 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      768 km
      1152 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
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      5 min
      9 min
    • Propellers
      1 qt
      3 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      3 qt
      5 qt
    • Guns
      2 qt
      4 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      800 kg
      1200 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      297 qt
      447 qt
    • Price
      41 USD
      750000000 USD

Dornier Do 11

TypeAircraft
Company

Dornier Flugzeugwerke

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
18.8
88.7
Height (m)
0.6
 
5.5
50.1
Wings
Wing area (m2)
1.1
 
107.8
925
Wingspan (Beam) (m)
0.1
 
26.3
95
Weights
Empty weight (kg)
8
 
5,978
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,200
575,000
Capacity
Crew (per.)
1
 
4
112
Speeds
Max. Speed (km/h)
25
 
260
28,165
Сruise Speed (km/h)
52
 
225
3,087
at 1000 m
Fuel
Fuel Capacity (l)
23
 
1,545
320,000
Power
Total Power (hp)
0.4
 
1,300
60,000
2 powerplants 650 hp each
Performance
Service ceiling (m)
0.6
 
4,100
161,544
Range (Ferry range) (km)
4
 
960
40,700
with 1545 l of fuel
Dynamic Performance
Time to altitude (min)
0.6
 
36
105
to 3000 m
0.6
 
7
105
to 1000 m
Propellers
Propellers (qt)
1
 
2
8
Prop blade number (qt)
1
 
4
8
Combat
Guns (qt)
1
 
3
18
manually aimed 7.92 mm (0.312 in) MG 15 machine guns
Bombs weight (kg)
2
 
1,000
39,000
Stat
Number built (qt)
0
 
372
43,000
Introduction 1930
First flight 07.05.1932

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