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    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      11 m2
      17 m2
    • Wingspan (Beam)
      6 m
      11 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
      336 kg
      504 kg
    • Max. takeoff weight (Gross weight)
      520 kg
      780 kg
    • Loaded weight
      512 kg
      768 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      3 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      96 km/h
      144 km/h
    • Сruise Speed
      80 km/h
      120 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
      46 l
      70 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
      48 hp
      72 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      1280 m
      1920 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      1 qt
      18 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Dornier Libelle

TypeFlying boat
Company

Dornier Flugzeugwerke

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
7.2
88.7
Height (m)
0.6
 
2.3
50.1
Wings
Wing area (m2)
1.1
 
14
925
Wingspan (Beam) (m)
0.1
 
8.5
95
Weights
Empty weight (kg)
8
 
420
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
650
575,000
Loaded weight (kg)
5
 
640
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
2
400
Speeds
Max. Speed (km/h)
25
 
120
28,165
Сruise Speed (km/h)
52
 
100
3,087
Fuel
Fuel Capacity (l)
23
 
58.3
320,000
Power
Total Power (hp)
0.4
 
60
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
1,600
161,544
Stat
Number built (qt)
0
 
2
43,000
Introduction 1921
First flight 16.08.1921

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