Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      24 m2
      38 m2
    • Wingspan (Beam)
      11 m
      17 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
      1733 kg
      2600 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      2408 kg
      3614 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
      257 km/h
      387 km/h
    • Сruise Speed
      220 km/h
      330 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
      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
      580 hp
      870 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5888 m
      8834 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      560 km
      840 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
      430 m/min
      646 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
      3 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
      72 qt
      108 qt
    • Price
      22400 USD
      33600 USD

Douglas O-46

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Parasol

Monoplane

Geometry
Length (m)
1.9
 
10.5
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wing area (m2)
1.1
 
30.8
925
Wingspan (Beam) (m)
0.1
 
13.9
95
Weights
Empty weight (kg)
8
 
2,166.4
276,800
Loaded weight (kg)
5
 
3,011
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
322
28,165
Сruise Speed (km/h)
52
 
275
3,087
Power
Total Power (hp)
0.4
 
725
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
7,360.9
161,544
Range (Ferry range) (km)
4
 
700
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
538.0
36,000
Combat
Guns (qt)
1
 
2
18
.30 cal (7.62 mm) Browning machine guns (one wing mounted and one flexible)
Stat
Number built (qt)
0
 
90
43,000
Price (USD)
41.5
 
28,000
750.0 million
Introduction 1934
First flight 1935

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