Search filter

    • Year
      1906
      2018
    • Length
      12 m
      19 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
      10 m
      16 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
      1924 kg
      2888 kg
    • Max. takeoff weight (Gross weight)
      3374 kg
      5062 kg
    • Loaded weight
      5 kg
      242500 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
      208 km/h
      312 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
      718 l
      1078 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
      1252 hp
      1880 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3560 m
      5340 m
    • Static ceiling
      2767 m
      4151 m
    • Range (Ferry range)
      480 km
      720 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
      329 m/min
      494 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
      108 qt
      164 qt
    • Price
      41 USD
      750000000 USD

Bell 430

TypeHelicopter
Company

Bell Aircraft Corporation

Geometry
Length (m)
1.9
 
15.3
88.7
Height (m)
0.6
 
3.7
50.1
Rotors
Main rotor diameter (m)
1.2
 
12.8
62
Weights
Empty weight (kg)
8
 
2,406
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,218
575,000
Speeds
Max. Speed (km/h)
25
 
260
28,165
Fuel
Fuel Capacity (l)
23
 
898
320,000
Power
Total Power (hp)
0.4
 
1,566
60,000
Performance
Service ceiling (m)
0.6
 
4,450
161,544
Static ceiling (m)
3
 
3,459
5,485
Range (Ferry range) (km)
4
 
600
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
411.5
36,000
Stat
Number built (qt)
0
 
136
43,000
First flight 25.10.1994

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