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    • Year
      1906
      2018
    • Length
      33 m
      50 m
    • Height
      10 m
      16 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      180 m2
      272 m2
    • Wingspan (Beam)
      31 m
      48 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
      35730 kg
      53596 kg
    • Max. takeoff weight (Gross weight)
      117026 kg
      175541 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      72560 kg
      90700 kg
    • Payload
      30118 kg
      45178 kg
    • Capacity passengers
      29 per.
      45 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      746 km/h
      1120 km/h
    • Сruise Speed
      710 km/h
      1066 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
      86047 l
      129071 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
      0 hp
      60000 hp
    • Thrust
      307 kN
      462 kN
    • Service ceiling
      12192 m
      18288 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1935 km
      2903 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
      1194 m/min
      1793 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
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      642 qt
      964 qt
    • Price
      31680000 USD
      47520000 USD

Boeing KC-135 Stratotanker

TypeAircraft
Company

Boeing

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
41.5
88.7
Height (m)
0.6
 
12.7
50.1
Wings
Wing area (m2)
1.1
 
226.0
925
Wingspan (Beam) (m)
0.1
 
39.9
95
Weights
Empty weight (kg)
8
 
44,663
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
146,283.5
575,000
Capacity
Crew (per.)
1
 
3
112
pilot, co-pilot and boom operator
Useful load (kg)
26.4
 
90,700
90,700
Payload (kg)
23
 
37,648.2
122,470
Capacity passengers (per.)
1
 
37
400
Speeds
Max. Speed (km/h)
25
 
933
28,165
Сruise Speed (km/h)
52
 
888
3,087
at 9144 m
Fuel
Fuel Capacity (l)
23
 
107,558.8
320,000
Power
Thrust (kN)
1.5
 
384.8
1,914
4 powerplants 96,2 each
Performance
Service ceiling (m)
0.6
 
15,240
161,544
Range (Ferry range) (km)
4
 
2,419
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,493.5
36,000
Stat
Number built (qt)
0
 
803
43,000
Price (USD)
41.5
 
39.6 million
750.0 million
Introduction 1956
First flight 31.08.1956
Stop production 2009

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