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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)
      20 m
      31 m
    • Wing loading
      68 kg/m2
      103 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
      4480 kg
      6720 kg
    • Max. takeoff weight (Gross weight)
      7360 kg
      11040 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
      168 km/h
      252 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
      1200 hp
      1800 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3360 m
      5040 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1200 km
      1800 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
      216 m/min
      324 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
      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
      225 qt
      339 qt
    • Price
      41 USD
      750000000 USD

Dornier Do 23

TypeAircraft
Company

Dornier Flugzeugwerke

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
18.8
88.7
Height (m)
0.6
 
5.4
50.1
Wings
Wing area (m2)
1.1
 
108
925
Wingspan (Beam) (m)
0.1
 
25.6
95
Wing loading (kg/m2)
3.1
 
85.2
829
Weights
Empty weight (kg)
8
 
5,600
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
9,200
575,000
Capacity
Crew (per.)
1
 
4
112
Speeds
Max. Speed (km/h)
25
 
260
28,165
Сruise Speed (km/h)
52
 
210
3,087
Power
Total Power (hp)
0.4
 
1,500
60,000
2 powerplants 750 hp each
Performance
Service ceiling (m)
0.6
 
4,200
161,544
Range (Ferry range) (km)
4
 
1,500
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
270
36,000
Combat
Guns (qt)
1
 
3
18
7.92 mm (.312 in) MG 15 machine guns (nose, dorsal and ventral positions)
Bombs weight (kg)
2
 
1,000
39,000
bombs carried internally
Stat
Number built (qt)
0
 
282
43,000
Introduction 1934
First flight 1934

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