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    • Year
      1906
      2018
    • Length
      26 m
      40 m
    • Height
      6 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      28 m
      43 m
    • Wing loading
      363 kg/m2
      546 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
      28693 kg
      43041 kg
    • Max. takeoff weight (Gross weight)
      83440 kg
      125160 kg
    • Loaded weight
      48272 kg
      72408 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
      781 km/h
      1173 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      153 kN
      231 kN
    • Service ceiling
      8071 m
      12107 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      1136 m/min
      1705 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
      22 qt
      34 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
      1625 qt
      2439 qt
    • Price
      1520000 USD
      2280000 USD

Boeing B-47 Stratojet

TypeAircraft
Company

Boeing

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
32.7
88.7
Height (m)
0.6
 
8.5
50.1
Wings
Wingspan (Beam) (m)
0.1
 
35.4
95
Wing loading (kg/m2)
3.1
 
454.8
829
Weights
Empty weight (kg)
8
 
35,867
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
104,300
575,000
Loaded weight (kg)
5
 
60,340
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
977
28,165
Power
Thrust/weight (kN/kg)
0.0
 
0.2
2.1
Thrust (kN)
1.5
 
192
1,914
6 powerplants 32 kN each
Performance
Service ceiling (m)
0.6
 
10,088.9
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,420.4
36,000
Combat
Guns (qt)
1
 
2
18
20 mm (0.787 in) M24A1 autocannons in a remote controlled tail turret
Bombs (qt)
1
 
2
250
Mk15 nuclear bombs or
1
 
1
250
B41 nuclear bomb or B53 nuclear bomb or
1
 
28
250
227 kg conventional bombs
Stat
Number built (qt)
0
 
2,032
43,000
Price (USD)
41.5
 
1.9 million
750.0 million
Introduction 1947
First flight 17.12.1947
Stop production 1969

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