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    • Year
      1906
      2018
    • Length
      17 m
      27 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      83 m2
      126 m2
    • Wingspan (Beam)
      21 m
      33 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
      8480 kg
      12720 kg
    • Max. takeoff weight (Gross weight)
      14720 kg
      22080 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      8 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
      272 km/h
      408 km/h
    • Сruise Speed
      211 km/h
      317 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
      1196 l
      1794 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
      2256 hp
      3384 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5040 m
      7560 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2160 km
      3240 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      2320 km
      3480 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
      268 m/min
      402 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      16 min
      26 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      2 qt
      4 qt
    • Bombs
      1 qt
      250 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
      223 qt
      335 qt
    • Price
      41 USD
      750000000 USD

Dornier Do 24

TypeFlying boat
Company

Dornier Flugzeugwerke

Scheme

Monoplane

Parasol

Geometry
Length (m)
1.9
 
21.9
88.7
Height (m)
0.6
 
5.8
50.1
Wings
Wing area (m2)
1.1
 
104.6
925
Wingspan (Beam) (m)
0.1
 
27
95
Weights
Empty weight (kg)
8
 
10,600
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
18,400
575,000
Capacity
Crew (per.)
1
 
6
112
Speeds
Max. Speed (km/h)
25
 
340
28,165
at 4800 m
Сruise Speed (km/h)
52
 
264
3,087
at 5400 m
Fuel
Fuel Capacity (l)
23
 
1,495
320,000
Power
Total Power (hp)
0.4
 
2,820
60,000
3 powerplants 940 hp each
Performance
Service ceiling (m)
0.6
 
6,300
161,544
Range (Ferry range) (km)
4
 
2,700
40,700
Сombat radius (km)
277
 
2,900
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
335
36,000
Time to altitude (min)
0.6
 
4.5
105
to 1000 m
0.6
 
21
105
to 4000 m
Combat
Guns (qt)
1
 
3
18
1 × 20 mm Hispano-Suiza HS.404 cannon; 2 × 7.92 mm (.312 in) MG 15 machine guns
Stat
Number built (qt)
0
 
279
43,000
Introduction 1983
First flight 03.07.1937

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