Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      36 m2
      54 m2
    • Wingspan (Beam)
      12 m
      20 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
      2080 kg
      3120 kg
    • Max. takeoff weight (Gross weight)
      3200 kg
      4800 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 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
      280 km/h
      420 km/h
    • Сruise Speed
      240 km/h
      360 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
      687 hp
      1032 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7200 m
      10800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1840 km
      2760 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
      384 m/min
      576 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      10 min
      16 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
      3 qt
      5 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      2 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      24 qt
      36 qt
    • Price
      41 USD
      750000000 USD

Dornier Do 22

TypeAircraft
Company

Dornier Flugzeugwerke

Scheme

Monoplane

Parasol

Geometry
Length (m)
1.9
 
13.1
88.7
Height (m)
0.6
 
4.9
50.1
Wings
Wing area (m2)
1.1
 
45
925
Wingspan (Beam) (m)
0.1
 
16.2
95
Weights
Empty weight (kg)
8
 
2,600
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,000
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
350
28,165
at 3000 m
Сruise Speed (km/h)
52
 
300
3,087
Power
Total Power (hp)
0.4
 
859.3
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
9,000
161,544
Range (Ferry range) (km)
4
 
2,300
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
480
36,000
Time to altitude (min)
0.6
 
13
105
to 5000 m
Combat
Guns (qt)
1
 
3
18
2 × 7.92 mm (.312 in) MG 15 machine guns in ventral and dorsal positions, 1 × 7.92 mm (.312 in) MG 17 machine gun in the nose
Bombs (qt)
1
 
4
250
50 kg (110 lb) bombs or
Torpedoes (qt)
1
 
1
4
00 kg (1,764 lb) torpedo
Stat
Number built (qt)
0
 
30
43,000
Introduction 1935
First flight 15.07.1938

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