Search filter

    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      71 m2
      108 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
      5922 kg
      8884 kg
    • Max. takeoff weight (Gross weight)
      10041 kg
      15063 kg
    • Loaded weight
      8692 kg
      13040 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
      278 km/h
      418 km/h
    • Сruise Speed
      215 km/h
      323 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
      1600 hp
      2400 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5827 m
      8742 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1160 km
      1740 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
      7 min
      12 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
      1600 kg
      2400 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      280 qt
      420 qt
    • Price
      46800 USD
      70200 USD

Douglas B-18 Bolo

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
17.6
88.7
Height (m)
0.6
 
4.6
50.1
Wings
Wing area (m2)
1.1
 
89.7
925
Wingspan (Beam) (m)
0.1
 
27.3
95
Weights
Empty weight (kg)
8
 
7,402.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
12,552.3
575,000
Loaded weight (kg)
5
 
10,866
242,500
Capacity
Crew (per.)
1
 
6
112
Speeds
Max. Speed (km/h)
25
 
348
28,165
at 3050
Сruise Speed (km/h)
52
 
269
3,087
Power
Total Power (hp)
0.4
 
2,000
60,000
2 powerplants 1000 each
Performance
Service ceiling (m)
0.6
 
7,284.7
161,544
Range (Ferry range) (km)
4
 
1,450
40,700
Dynamic Performance
Time to altitude (min)
0.6
 
9.9
105
to 3050
Combat
Guns (qt)
1
 
3
18
.30 in (7.62 mm) machine guns
Bombs weight (kg)
2
 
2,000
39,000
Stat
Number built (qt)
0
 
350
43,000
Price (USD)
41.5
 
58,500
750.0 million
Introduction 1935
First flight 01.04.1935
Stop production 1946

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