Search filter

    • Year
      1906
      2018
    • Length
      18 m
      28 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      87 m2
      132 m2
    • Wingspan (Beam)
      21 m
      33 m
    • Wing loading
      282 kg/m2
      425 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
      16581 kg
      24872 kg
    • Max. takeoff weight (Gross weight)
      39916 kg
      59875 kg
    • Loaded weight
      29544 kg
      44316 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
      736 km/h
      1104 km/h
    • Сruise Speed
      644 km/h
      966 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      80 kN
      120 kN
    • Service ceiling
      11314 m
      16972 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1288 km
      1932 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
      1450 m/min
      2177 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
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      880000 USD
      1320000 USD

North American Aviation B-45 Tornado

TypeAircraft
Company

North American Aviation

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
23.0
88.7
Height (m)
0.6
 
7.7
50.1
Wings
Wing area (m2)
1.1
 
109.2
925
Wingspan (Beam) (m)
0.1
 
27.1
95
Wing loading (kg/m2)
3.1
 
353.4
829
Weights
Empty weight (kg)
8
 
20,726.5
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
49,895.2
575,000
Loaded weight (kg)
5
 
36,930
242,500
Capacity
Crew (per.)
1
 
4
112
Pilot, Co-Pilot, Bombardier-Navigator and Tail Gunner
Speeds
Max. Speed (km/h)
25
 
920
28,165
Сruise Speed (km/h)
52
 
805
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.3
2.1
Thrust (kN)
1.5
 
100
1,914
4 powerplants 25 kN
Performance
Service ceiling (m)
0.6
 
14,142.7
161,544
Range (Ferry range) (km)
4
 
1,610
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,813.6
36,000
Combat
Guns (qt)
1
 
2
18
.50 in (12.7 mm) M3 machine guns (Defensive)
Stat
Price (USD)
41.5
 
1.1 million
750.0 million
Introduction 1947
First flight 17.03.1947
Stop production 1959

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