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
      1 m2
      925 m2
    • Wingspan (Beam)
      14 m
      22 m
    • Wing loading
      124 kg/m2
      188 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
      4168 kg
      6252 kg
    • Max. takeoff weight (Gross weight)
      7069 kg
      10605 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
      280 km/h
      420 km/h
    • Max. Speed
      328 km/h
      492 km/h
    • Сruise Speed
      240 km/h
      360 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
      1232 l
      1848 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6560 m
      9840 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      528 km
      792 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
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      3 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      2 qt
      4 qt
    • Guns
      4 qt
      8 qt
    • Bombs
      3 qt
      5 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
      1711 qt
      2567 qt
    • Price
      41 USD
      750000000 USD

Dornier Do 17

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
Wingspan (Beam) (m)
0.1
 
18
95
Wing loading (kg/m2)
3.1
 
156
829
Weights
Empty weight (kg)
8
 
5,210
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,837
575,000
Capacity
Crew (per.)
1
 
4
112
Speeds
Ground Speed (km/h)
96.6
 
350
1,500
at 8040 kg
Max. Speed (km/h)
25
 
410
28,165
at 8040 kg at 5000 m
Сruise Speed (km/h)
52
 
300
3,087
at 8837 kg at 4000 m
Fuel
Fuel Capacity (l)
23
 
1,540
320,000
Power
Power/mass (hp/kg)
0.0
 
0.2
22.1
Performance
Service ceiling (m)
0.6
 
8,200
161,544
Сombat radius (km)
277
 
660
7,210
with 1540 l fuel and 1000 kg of bombs
Propellers
Propellers (qt)
1
 
2
8
Prop blade number (qt)
1
 
3
8
Combat
Guns (qt)
1
 
6
18
7.92 mm (0.312 in) MG 15 machine guns in front, rear upper, rear lower and cockpit side positions
Bombs (qt)
1
 
20
250
50 kg bombs or
1
 
4
250
250 kg (551 lb) bombs
Stat
Number built (qt)
0
 
2,139
43,000
Introduction 1934
First flight 23.11.1934
Stop production 15.09.1952

Similar aircraft

Get more

Museums on map

Museums

Comments