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    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 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
      8291 kg
      12438 kg
    • Max. takeoff weight (Gross weight)
      12700 kg
      19051 kg
    • Loaded weight
      10015 kg
      15023 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
      456 km/h
      684 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
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      3200 hp
      4800 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5364 m
      8047 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1840 km
      2760 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
      304 m/min
      458 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
      18 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      8 qt
      12 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2160 kg
      3240 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1961 qt
      2943 qt
    • Price
      194076 USD
      291114 USD

Douglas A-26 Invader

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
15.2
88.7
Height (m)
0.6
 
5.6
50.1
Wings
Wingspan (Beam) (m)
0.1
 
21.4
95
Weights
Empty weight (kg)
8
 
10,364.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
15,875.7
575,000
Loaded weight (kg)
5
 
12,519
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
570
28,165
Power
Total Power (hp)
0.4
 
4,000
60,000
2 powerplants 2000 each
Performance
Service ceiling (m)
0.6
 
6,705.6
161,544
Range (Ferry range) (km)
4
 
2,300
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
381
36,000
Combat
Rockets (qt)
1
 
10
76
5-inch (12.7 cm) HVAR rockets on "zero length" launch pylons, five under each outer wing panel
Bombs weight (kg)
2
 
2,700
39,000
Stat
Number built (qt)
0
 
2,452
43,000
Price (USD)
41.5
 
242,595
750.0 million
Introduction 1942
First flight 10.07.1942
Stop production 1980

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