Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 m2
    • Wingspan (Beam)
      10 m
      16 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
      1456 kg
      2184 kg
    • Max. takeoff weight (Gross weight)
      2000 kg
      3000 kg
    • Loaded weight
      1919 kg
      2880 kg
    • Crew
      1 per.
      3 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
      232 km/h
      348 km/h
    • Сruise Speed
      195 km/h
      293 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      29 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
      432 hp
      648 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5200 m
      7800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      320 km
      480 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
      3 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      2 qt
      4 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Dornier Do 29

TypeAircraft
Company

Dornier Flugzeugwerke

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
9.5
88.7
Height (m)
0.6
 
2.7
50.1
Wings
Wing area (m2)
1.1
 
21.8
925
Wingspan (Beam) (m)
0.1
 
13.2
95
Weights
Empty weight (kg)
8
 
1,820
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,500
575,000
Loaded weight (kg)
5
 
2,400.0
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
290
28,165
Сruise Speed (km/h)
52
 
244
3,087
Minimum control speed (km/h)
24
 
24
113
Power
Total Power (hp)
0.4
 
540
60,000
2 powerplants 270 hp each
Performance
Service ceiling (m)
0.6
 
6,500
161,544
Range (Ferry range) (km)
4
 
400
40,700
Propellers
Propellers (qt)
1
 
2
8
Prop blade number (qt)
1
 
3
8
Stat
Introduction 1958
First flight 12.12.1958

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