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    • Year
      1906
      2018
    • Length
      13 m
      20 m
    • Height
      4 m
      7 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
      11 m
      18 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
      4118 kg
      6178 kg
    • Max. takeoff weight (Gross weight)
      6894 kg
      10342 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      2177 kg
      3266 kg
    • Payload
      2177 kg
      3266 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      160 km/h
      240 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
      2344 hp
      3516 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2926 m
      4390 m
    • Static ceiling
      1960 m
      2940 m
    • Range (Ferry range)
      576 km
      864 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
      207 m/min
      311 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
      20 qt
      32 qt
    • Price
      41 USD
      750000000 USD

Bristol Type 192 Belvedere

TypeHelicopter
Company

Bristol Aeroplane Company

Geometry
Length (m)
1.9
 
16.6
88.7
Height (m)
0.6
 
5.2
50.1
Rotors
Main rotor diameter (m)
1.2
 
14.9
62
Weights
Empty weight (kg)
8
 
5,148.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,618.3
575,000
Capacity
Crew (per.)
1
 
3
112
Useful load (kg)
26.4
 
2,721.6
90,700
Payload (kg)
23
 
2,721.6
122,470
Speeds
Сruise Speed (km/h)
52
 
200
3,087
Power
Total Power (hp)
0.4
 
1,463.8
60,000
0.4
 
2,930
60,000
2 powerplants 1465 hp each
Performance
Service ceiling (m)
0.6
 
3,657.6
161,544
Static ceiling (m)
3
 
2,450
5,485
Range (Ferry range) (km)
4
 
720
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
259.1
36,000
Stat
Number built (qt)
0
 
26
43,000
Introduction 1958
First flight 05.07.1958
Stop production 1969

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