Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      2 m
      5 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
      13 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
      1 m
      2 m
    • Empty weight
      968 kg
      1453 kg
    • Max. takeoff weight (Gross weight)
      2177 kg
      3266 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      960 kg
      1440 kg
    • Payload
      960 kg
      1440 kg
    • Capacity passengers
      4 per.
      6 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      208 km/h
      312 km/h
    • Сruise Speed
      196 km/h
      296 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
      444 l
      668 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
      649 hp
      975 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4557 m
      6837 m
    • Static ceiling
      2974 m
      4462 m
    • Range (Ferry range)
      480 km
      721 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      3 h
      6 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
      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
      865 qt
      1299 qt
    • Price
      2032000 USD
      3048000 USD

Bell 407

TypeHelicopter
Company

Bell Aircraft Corporation

Geometry
Length (m)
1.9
 
12.7
88.7
Height (m)
0.6
 
3.6
50.1
Rotors
Main rotor diameter (m)
1.2
 
10.7
62
Tail rotor diameter (m)
0.8
 
1.7
4.9
Weights
Empty weight (kg)
8
 
1,210.2
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,721.6
575,000
Capacity
Crew (per.)
1
 
1
112
Useful load (kg)
26.4
 
1,200
90,700
Payload (kg)
23
 
1,200
122,470
Capacity passengers (per.)
1
 
5
400
Speeds
Max. Speed (km/h)
25
 
260
28,165
Сruise Speed (km/h)
52
 
246
3,087
Fuel
Fuel Capacity (l)
23
 
556
320,000
Power
Total Power (hp)
0.4
 
812.3
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,696.7
161,544
Static ceiling (m)
3
 
3,718
5,485
Range (Ferry range) (km)
4
 
600.1
40,700
Endurance (h)
0.0
 
4.2
150
Stat
Number built (qt)
0
 
1,082
43,000
Price (USD)
41.5
 
2.5 million
750.0 million
Introduction 1994
First flight 29.06.1995

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