Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      73 m2
      110 m2
    • Wingspan (Beam)
      14 m
      22 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
      1888 kg
      2832 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      3312 kg
      4968 kg
    • Crew
      1 per.
      3 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
      154 km/h
      232 km/h
    • Сruise Speed
      129 km/h
      195 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
      520 hp
      780 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4364 m
      6548 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1108 km
      1662 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      9 h
      15 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
      2 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      181 kg
      273 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      2 qt
      4 qt
    • Price
      41 USD
      750000000 USD

Bristol Type 90 Berkeley

TypeAircraft
Company

Bristol Aeroplane Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
14.5
88.7
Height (m)
0.6
 
4.3
50.1
Wings
Wing area (m2)
1.1
 
91.5
925
Wingspan (Beam) (m)
0.1
 
17.7
95
Weights
Empty weight (kg)
8
 
2,360
276,800
Loaded weight (kg)
5
 
4,140
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
193
28,165
Сruise Speed (km/h)
52
 
162
3,087
Power
Total Power (hp)
0.4
 
650
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,456
161,544
Range (Ferry range) (km)
4
 
1,385
40,700
Endurance (h)
0.0
 
12
150
Combat
Guns (qt)
1
 
1
18
0.303 in (7.7 mm) Lewis gun in rear cockpit
Bombs weight (kg)
2
 
227
39,000
Stat
Number built (qt)
0
 
3
43,000
Introduction 1925
First flight 05.03.1925

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