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    • Year
      1906
      2018
    • Length
      19 m
      30 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      96 m2
      144 m2
    • Wingspan (Beam)
      24 m
      36 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
      8160 kg
      12240 kg
    • Max. takeoff weight (Gross weight)
      16000 kg
      24000 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      400 kg
      600 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      268 km/h
      402 km/h
    • Сruise Speed
      248 km/h
      372 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
      1920 hp
      2880 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3680 m
      5520 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      7200 km
      10800 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      3824 km
      5736 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
      100 m/min
      150 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
      1 qt
      18 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      4 qt
      8 qt
    • Price
      41 USD
      750000000 USD

Dornier Do 26

TypeFlying boat
Company

Dornier Flugzeugwerke

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
24.6
88.7
Height (m)
0.6
 
6.9
50.1
Wings
Wing area (m2)
1.1
 
120
925
Wingspan (Beam) (m)
0.1
 
30
95
Weights
Empty weight (kg)
8
 
10,200
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
20,000
575,000
Capacity
Crew (per.)
1
 
4
112
Payload (kg)
23
 
500
122,470
Speeds
Max. Speed (km/h)
25
 
335
28,165
Сruise Speed (km/h)
52
 
310
3,087
Power
Total Power (hp)
0.4
 
2,400
60,000
4 powerplants 600 hp each
Performance
Service ceiling (m)
0.6
 
4,600
161,544
Range (Ferry range) (km)
4
 
9,000
40,700
Сombat radius (km)
277
 
4,780
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
125
36,000
Stat
Number built (qt)
0
 
6
43,000
Introduction 1938
First flight 21.05.1938
Stop production 1945

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