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    • Year
      1906
      2018
    • Length
      20 m
      31 m
    • Height
      7 m
      12 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      105 m2
      159 m2
    • Wingspan (Beam)
      32 m
      50 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
      21873 kg
      32810 kg
    • Max. takeoff weight (Gross weight)
      44724 kg
      67087 kg
    • Loaded weight
      36640 kg
      54960 kg
    • Crew
      8 per.
      12 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
      460 km/h
      690 km/h
    • Сruise Speed
      373 km/h
      561 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
      7040 hp
      10560 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7485 m
      11229 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4894 km
      7342 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
      256 m/min
      385 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
      8 qt
      12 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      7280 kg
      10920 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      94 qt
      142 qt
    • Price
      41 USD
      750000000 USD

Consolidated B-32 Dominator

TypeAircraft
Company

Consolidated Aircraft Corporation

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
25.0
88.7
Height (m)
0.6
 
9.8
50.1
Wings
Wing area (m2)
1.1
 
132.1
925
Wingspan (Beam) (m)
0.1
 
41.2
95
Weights
Empty weight (kg)
8
 
27,341.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
55,905.3
575,000
Loaded weight (kg)
5
 
45,800
242,500
Capacity
Crew (per.)
1
 
10
112
Speeds
Max. Speed (km/h)
25
 
575
28,165
at 9150
Сruise Speed (km/h)
52
 
467
3,087
Power
Total Power (hp)
0.4
 
8,800
60,000
4 powerplants 2200 hp each
Performance
Service ceiling (m)
0.6
 
9,357.4
161,544
Range (Ferry range) (km)
4
 
6,118
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
320.0
36,000
Combat
Guns (qt)
1
 
10
18
.50 in (12.7 mm) machine guns
Bombs weight (kg)
2
 
9,100
39,000
Stat
Number built (qt)
0
 
118
43,000
Introduction 1942
First flight 07.09.1942
Stop production 30.08.1945

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