Search filter

    • Year
      1906
      2018
    • Length
      13 m
      20 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      41 m2
      62 m2
    • Wingspan (Beam)
      56 m
      84 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
      7579 kg
      11370 kg
    • Max. takeoff weight (Gross weight)
      12955 kg
      19433 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
      528 km/h
      792 km/h
    • Сruise Speed
      401 km/h
      603 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
      2120 hp
      3180 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7168 m
      10754 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2316 km
      3474 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      2317 km
      3477 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
      0 min
      105 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      4 qt
      8 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2903 kg
      4355 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      10960000 USD
      16440000 USD

Douglas XB-42 Mixmaster

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
16.4
88.7
Height (m)
0.6
 
5.7
50.1
Wings
Wing area (m2)
1.1
 
51.6
925
Wingspan (Beam) (m)
0.1
 
70
95
Weights
Empty weight (kg)
8
 
9,474.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
16,194.2
575,000
Capacity
Crew (per.)
1
 
3
112
pilot, copilot/gunner and bombardier
Speeds
Max. Speed (km/h)
25
 
660
28,165
at 7145
Сruise Speed (km/h)
52
 
502
3,087
Power
Total Power (hp)
0.4
 
2,650
60,000
2 powerplants 1325 hp each
Performance
Service ceiling (m)
0.6
 
8,961.1
161,544
Range (Ferry range) (km)
4
 
2,895
40,700
Сombat radius (km)
277
 
2,897
7,210
Combat
Guns (qt)
1
 
6
18
.50 in (12.7 mm) machine guns, two twin rear-firing turrets and two fixed forward-firin
Bombs weight (kg)
2
 
3,629
39,000
Stat
Number built (qt)
0
 
2
43,000
Price (USD)
41.5
 
13.7 million
750.0 million
Introduction 1944
First flight 06.05.1944

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