Search filter

    • Year
      1906
      2018
    • Length
      18 m
      28 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      57 m2
      87 m2
    • Wingspan (Beam)
      17 m
      27 m
    • Wing loading
      289 kg/m2
      434 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
      15436 kg
      23155 kg
    • Max. takeoff weight (Gross weight)
      30118 kg
      45178 kg
    • Loaded weight
      20960 kg
      31440 kg
    • Crew
      2 per.
      4 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
      816 km/h
      1224 km/h
    • Сruise Speed
      52 km/h
      3087 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      72 kN
      108 kN
    • Service ceiling
      9607 m
      14411 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3176 km
      4764 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1200 km
      1800 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
      1219 m/min
      1829 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
      5443 kg
      8165 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      235 qt
      353 qt
    • Price
      2040000 USD
      3060000 USD

Douglas B-66 Destroyer

TypeAircraft
Company

Douglas Aircraft Company

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
22.9
88.7
Height (m)
0.6
 
7.2
50.1
Wings
Wing area (m2)
1.1
 
72.5
925
Wingspan (Beam) (m)
0.1
 
22.1
95
Wing loading (kg/m2)
3.1
 
361.4
829
Weights
Empty weight (kg)
8
 
19,295.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
37,648.2
575,000
Loaded weight (kg)
5
 
26,200
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
1,020
28,165
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
Thrust (kN)
1.5
 
90
1,914
2 powerplants 45 kN each
Performance
Service ceiling (m)
0.6
 
12,009.1
161,544
Range (Ferry range) (km)
4
 
3,970
40,700
Сombat radius (km)
277
 
1,500
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,524
36,000
Combat
Guns (qt)
1
 
2
18
1
 
2
18
20 mm M24 cannons in radar-controlled/remotely operated tail turret
Bombs weight (kg)
2
 
6,803.9
39,000
Stat
Number built (qt)
0
 
294
43,000
Price (USD)
41.5
 
2.6 million
750.0 million
Introduction 1954
First flight 28.06.1954
Stop production 1973

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