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    • Year
      1906
      2018
    • Length
      15 m
      24 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      78 m2
      118 m2
    • Wingspan (Beam)
      18 m
      29 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
      5344 kg
      8016 kg
    • Max. takeoff weight (Gross weight)
      6800 kg
      10200 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
      200 km/h
      300 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      152 km/h
      228 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
      968 hp
      1452 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3480 m
      5220 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2800 km
      4200 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
      104 m/min
      156 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
      2 qt
    • Bombs
      1 qt
      3 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
      136 qt
      204 qt
    • Price
      41 USD
      750000000 USD

Dornier Do 18

TypeFlying boat
Company

Dornier Flugzeugwerke

Scheme

Monoplane

Parasol

Geometry
Length (m)
1.9
 
19.2
88.7
Height (m)
0.6
 
5.3
50.1
Wings
Wing area (m2)
1.1
 
98
925
Wingspan (Beam) (m)
0.1
 
23.7
95
Weights
Empty weight (kg)
8
 
6,680
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,500
575,000
Normal take-off)
Capacity
Crew (per.)
1
 
4
112
Speeds
Ground Speed (km/h)
96.6
 
250
1,500
Сruise Speed (km/h)
52
 
190
3,087
Power
Total Power (hp)
0.4
 
1,210
60,000
2 powerplants 605 hp each
Performance
Service ceiling (m)
0.6
 
4,350
161,544
Range (Ferry range) (km)
4
 
3,500
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
130
36,000
Combat
Guns (qt)
1
 
1
18
7.92 mm MG 15 machine gun
Bombs (qt)
1
 
2
250
50 kg (110 lb) bombs under starboard wing
Stat
Number built (qt)
0
 
170
43,000
Introduction 1935
First flight 15.03.1935

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