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    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      76 m2
      116 m2
    • Wingspan (Beam)
      17 m
      27 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
      2904 kg
      4356 kg
    • Max. takeoff weight (Gross weight)
      5600 kg
      8400 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
      8 per.
      12 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      148 km/h
      222 km/h
    • Сruise Speed
      116 km/h
      174 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
      568 hp
      852 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2800 m
      4200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      640 km
      960 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
      72 m/min
      108 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      26 min
      40 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
      200 qt
      300 qt
    • Price
      41 USD
      750000000 USD

Dornier Do J

TypeFlying boat
Company

Dornier Flugzeugwerke

Scheme

Monoplane

Parasol

Geometry
Length (m)
1.9
 
17.3
88.7
Height (m)
0.6
 
5.6
50.1
Wings
Wing area (m2)
1.1
 
96
925
Wingspan (Beam) (m)
0.1
 
22
95
Weights
Empty weight (kg)
8
 
3,630
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,000
575,000
Capacity
Crew (per.)
1
 
3
112
Capacity passengers (per.)
1
 
10
400
Speeds
Max. Speed (km/h)
25
 
185
28,165
Сruise Speed (km/h)
52
 
145
3,087
Power
Total Power (hp)
0.4
 
710
60,000
2 powerplants 355 hp each
Performance
Service ceiling (m)
0.6
 
3,500
161,544
Range (Ferry range) (km)
4
 
800
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
90
36,000
Time to altitude (min)
0.6
 
33
105
to 3000 m
Stat
Number built (qt)
0
 
250
43,000
Introduction 1931
First flight 06.11.1922
Stop production 1950

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