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    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      54 m2
      82 m2
    • Wingspan (Beam)
      16 m
      25 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
      8 kg
      276800 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      16112 kg
      24168 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
      448 km/h
      672 km/h
    • Сruise Speed
      336 km/h
      504 km/h
    • Stall Speed
      106 km/h
      160 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
      2800 hp
      4200 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7840 m
      11760 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3200 km
      4800 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
      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
      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
      4 qt
      8 qt
    • Price
      41 USD
      750000000 USD

Dornier Do 317

TypeAircraft
Company

Dornier Flugzeugwerke

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
16.8
88.7
Height (m)
0.6
 
5.4
50.1
Wings
Wing area (m2)
1.1
 
68
925
Wingspan (Beam) (m)
0.1
 
20.6
95
Weights
Loaded weight (kg)
5
 
20,140
242,500
Capacity
Crew (per.)
1
 
4
112
Speeds
Max. Speed (km/h)
25
 
560
28,165
at 6000 m
Сruise Speed (km/h)
52
 
420
3,087
Stall Speed (km/h)
40
 
133
257.7
Power
Total Power (hp)
0.4
 
3,500
60,000
2 powerplants 1750 hp
Performance
Service ceiling (m)
0.6
 
9,800
161,544
Range (Ferry range) (km)
4
 
4,000
40,700
Combat
Guns (qt)
1
 
6
18
3 × 13 mm (0.512 in) MG 131 machine gun in upper turret, rear dorsal, and rear ventral positions; 2 × 7.92 mm (0.312 in) MG 81 machine gun in nose; 1 × 15 mm (0.591 in) MG 151 cannon in nose
Bombs weight (kg)
2
 
4,000
39,000
of disposable stores
Stat
Number built (qt)
0
 
6
43,000
Introduction 1943
First flight 01.09.1943

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