Search filter

    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      44 m2
      66 m2
    • Wingspan (Beam)
      14 m
      22 m
    • Wing loading
      84 kg/m2
      127 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
      4160 kg
      6240 kg
    • Max. takeoff weight (Gross weight)
      7080 kg
      10620 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
      273 km/h
      411 km/h
    • Max. Speed
      404 km/h
      608 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
      1854 hp
      2782 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7200 m
      10800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1960 km
      2940 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
      264 m/min
      396 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
      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
      84 qt
      126 qt
    • Price
      41 USD
      750000000 USD

Dornier Do 215

TypeAircraft
Company

Dornier Flugzeugwerke

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
15.8
88.7
Height (m)
0.6
 
4.6
50.1
Wings
Wing area (m2)
1.1
 
55
925
Wingspan (Beam) (m)
0.1
 
18
95
Wing loading (kg/m2)
3.1
 
105.1
829
Weights
Empty weight (kg)
8
 
5,200
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,850
575,000
Capacity
Crew (per.)
1
 
4
112
pilot, bomb aimer/gunner, two gunners
Speeds
Ground Speed (km/h)
96.6
 
342
1,500
Max. Speed (km/h)
25
 
506
28,165
at 4500 m
Power
Total Power (hp)
0.4
 
2,318
60,000
Performance
Service ceiling (m)
0.6
 
9,000
161,544
Range (Ferry range) (km)
4
 
2,450
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
330
36,000
Combat
Guns (qt)
1
 
4
18
7.92 mm (.312 in) MG 15 machine guns, later upgraded to 6
Bombs weight (kg)
2
 
1,000
39,000
Stat
Number built (qt)
0
 
105
43,000
Introduction 1939
First flight 1938
Stop production 1944

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