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    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      65 m2
      99 m2
    • Wingspan (Beam)
      13 m
      21 m
    • Wing loading
      46 kg/m2
      70 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
      2181 kg
      3272 kg
    • Max. takeoff weight (Gross weight)
      3818 kg
      5728 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 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
      160 km/h
      242 km/h
    • Сruise Speed
      148 km/h
      224 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
      840 hp
      1260 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3372 m
      5059 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      588 km
      883 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
      243 m/min
      366 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
      2 qt
    • Bombs weight
      587 kg
      881 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      24 qt
      38 qt
    • Price
      41 USD
      750000000 USD

Douglas T2D

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
12.8
88.7
Height (m)
0.6
 
4.9
50.1
Wings
Wing area (m2)
1.1
 
82.3
925
Wingspan (Beam) (m)
0.1
 
17.4
95
Wing loading (kg/m2)
3.1
 
58
829
Weights
Empty weight (kg)
8
 
2,726.5
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,773.2
575,000
Capacity
Crew (per.)
1
 
4
112
Speeds
Max. Speed (km/h)
25
 
201
28,165
Сruise Speed (km/h)
52
 
186
3,087
Power
Total Power (hp)
0.4
 
1,050
60,000
2 powerplants 525 hp each
Performance
Service ceiling (m)
0.6
 
4,215.4
161,544
Range (Ferry range) (km)
4
 
735.2
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
304.8
36,000
Combat
Guns (qt)
1
 
2
18
.30 in (7.62 mm) M1919 Browning machine guns
Torpedoes (qt)
1
 
1
4
734 kg torpedo or equivalent bombload
Bombs weight (kg)
2
 
734
39,000
or 1 torpedo
Stat
Number built (qt)
0
 
31
43,000
Introduction 1927
First flight 27.01.1927
Stop production 1937

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