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    • Year
      1906
      2018
    • Length
      11 m
      17 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      44 m2
      68 m2
    • Wingspan (Beam)
      17 m
      26 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
      6678 kg
      10019 kg
    • Max. takeoff weight (Gross weight)
      12613 kg
      18921 kg
    • Loaded weight
      5 kg
      242500 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
      436 km/h
      656 km/h
    • Сruise Speed
      216 km/h
      324 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
      2400 hp
      3600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5974 m
      8962 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1610 km
      2416 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
      338 m/min
      509 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
      5 qt
      9 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      3 qt
      4 qt
    • Bombs weight
      3048 kg
      4572 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Douglas TB2D Skypirate

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
14.0
88.7
Height (m)
0.6
 
6.9
50.1
Wings
Wing area (m2)
1.1
 
56.2
925
Wingspan (Beam) (m)
0.1
 
21.3
95
Weights
Empty weight (kg)
8
 
8,348.4
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
15,766.9
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
546
28,165
Сruise Speed (km/h)
52
 
270
3,087
Power
Total Power (hp)
0.4
 
3,000
60,000
1powerplant
Performance
Service ceiling (m)
0.6
 
7,467.6
161,544
Range (Ferry range) (km)
4
 
2,013
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
423.7
36,000
Combat
Guns (qt)
1
 
7
18
4 × wing mounted .50 in (12.7 mm) machine guns; 2 × .50 in (12.7 mm) machine guns in dorsal turret; 1 × .50 in machine gun in ventral bath
Torpedoes (qt)
1
 
4
4
Bombs weight (kg)
2
 
3,810
39,000
or
Stat
Number built (qt)
0
 
2
43,000
Introduction 1945
First flight 13.03.1945

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