Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      0 m
      51 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      0 m
      95 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
      8 m
      14 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
      907 kg
      1361 kg
    • Max. takeoff weight (Gross weight)
      2358 kg
      3538 kg
    • Loaded weight
      2358 kg
      3538 kg
    • Crew
      1 per.
      112 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
      206 km/h
      310 km/h
    • Сruise Speed
      208 km/h
      312 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
      440 hp
      660 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7320 m
      10980 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
      16 h
      24 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      9
    • Load factor from
      2 G
      9 G
    • Rate of climb
      1 m/min
      36000 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Boeing A160 Hummingbird

TypeHelicopter
Company

Boeing

Scheme

Unmanned

Geometry
Length (m)
1.9
 
10.7
88.7
Rotors
Main rotor diameter (m)
1.2
 
11
62
Weights
Empty weight (kg)
8
 
1,134
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,948
575,000
Loaded weight (kg)
5
 
2,948
242,500
Speeds
Max. Speed (km/h)
25
 
258
28,165
Сruise Speed (km/h)
52
 
260
3,087
Power
Total Power (hp)
0.4
 
550
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
9,150
161,544
Endurance (h)
0.0
 
20
150
or more
Maximum glide ratio
7
 
7
43
according to Karem
Stat
Introduction 2007
First flight 2002

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