Search filter

    • 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
      63502 kg
      95255 kg
    • Max. takeoff weight (Gross weight)
      117026 kg
      175541 kg
    • Loaded weight
      108000 kg
      162000 kg
    • Crew
      21 per.
      33 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
      746 km/h
      1120 km/h
    • Сruise Speed
      688 km/h
      1032 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
      0 hp
      60000 hp
    • Thrust
      307 kN
      461 kN
    • Service ceiling
      12192 m
      18288 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4440 km
      6660 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
      25 qt
      39 qt
    • Price
      41 USD
      750000000 USD

Boeing RC-135

TypeAircraft
Company

Boeing

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
41.4
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
 
79,378.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
146,283.5
575,000
Loaded weight (kg)
5
 
135,000
242,500
Capacity
Crew (per.)
1
 
27
112
3 pilots, 2 navigators, 22 rear-crew members
Speeds
Max. Speed (km/h)
25
 
933
28,165
Сruise Speed (km/h)
52
 
860
3,087
Power
Thrust (kN)
1.5
 
384
1,914
4 powerplants 96 kN each
Performance
Service ceiling (m)
0.6
 
15,240
161,544
Range (Ferry range) (km)
4
 
5,550
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,493.5
36,000
Stat
Number built (qt)
0
 
32
43,000
Introduction 1964

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