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    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      88 m2
      134 m2
    • Wingspan (Beam)
      22 m
      34 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
      5088 kg
      7632 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      6800 kg
      10200 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
      200 km/h
      300 km/h
    • Сruise Speed
      52 km/h
      3087 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
      4800 m
      7200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      129 m/min
      195 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
      3 qt
      5 qt
    • Bombs
      9 qt
      15 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
      3 qt
      5 qt
    • Price
      41 USD
      750000000 USD

Dornier Do Y

Company

Dornier Flugzeugwerke

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
18.2
88.7
Height (m)
0.6
 
6.8
50.1
Wings
Wing area (m2)
1.1
 
111
925
Wingspan (Beam) (m)
0.1
 
28
95
Weights
Empty weight (kg)
8
 
6,360
276,800
Loaded weight (kg)
5
 
8,500
242,500
Capacity
Crew (per.)
1
 
4
112
Speeds
Max. Speed (km/h)
25
 
250
28,165
Power
Total Power (hp)
0.4
 
1,500
60,000
3 powerplants 500 hp each
Performance
Service ceiling (m)
0.6
 
6,000
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
162
36,000
Combat
Guns (qt)
1
 
4
18
2 × trainable machine guns in open position in nose; 2 × trainable machine guns in open dorsal position
Bombs (qt)
1
 
12
250
100 kg (220 lb) bombs
Stat
Number built (qt)
0
 
4
43,000
First flight 01.03.1930

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