Search filter

    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      45 m2
      69 m2
    • Wingspan (Beam)
      15 m
      23 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
      7280 kg
      10920 kg
    • Max. takeoff weight (Gross weight)
      13360 kg
      20040 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
      349 km/h
      525 km/h
    • Max. Speed
      445 km/h
      669 km/h
    • Сruise Speed
      320 km/h
      480 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
      2761 hp
      4143 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5896 m
      8844 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1716 km
      2574 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
      168 m/min
      252 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
      4 qt
      8 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      3200 kg
      4800 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1540 qt
      2310 qt
    • Price
      41 USD
      750000000 USD

Dornier Do 217

TypeAircraft
Company

Dornier Flugzeugwerke

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
17
88.7
Height (m)
0.6
 
5.0
50.1
Wings
Wing area (m2)
1.1
 
57
925
Wingspan (Beam) (m)
0.1
 
19
95
Weights
Empty weight (kg)
8
 
9,100
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
16,700
575,000
Capacity
Crew (per.)
1
 
4
112
Speeds
Ground Speed (km/h)
96.6
 
437
1,500
Max. Speed (km/h)
25
 
557
28,165
at 5700 m
Сruise Speed (km/h)
52
 
400
3,087
Power
Total Power (hp)
0.4
 
3,452
60,000
2 powerplants 1726 hp each
Performance
Service ceiling (m)
0.6
 
7,370
161,544
Range (Ferry range) (km)
4
 
2,145
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
210
36,000
Combat
Guns (qt)
1
 
6
18
4 × 7.92 mm (.312 in) MG 81 machine guns in nose and lateral positions; 2 × 13 mm (.51 in) MG 131 machine guns in dorsal and ventral positions
Bombs weight (kg)
2
 
4,000
39,000
internally & externally
Stat
Number built (qt)
0
 
1,925
43,000
Introduction 1941
First flight 04.10.1938
Stop production 1945

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