Search filter

    • Year
      1906
      2018
    • Length
      7 m
      11 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      33 m2
      51 m2
    • Wingspan (Beam)
      9 m
      14 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
      351 kg
      528 kg
    • Max. takeoff weight (Gross weight)
      604 kg
      907 kg
    • Loaded weight
      5 kg
      242500 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
      90 km/h
      136 km/h
    • Сruise Speed
      65 km/h
      99 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
      80 hp
      120 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      0 m
      161544 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
      4 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
      8 min
      14 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
      9 qt
      15 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
      29 qt
      45 qt
    • Price
      41 USD
      750000000 USD

Bristol Bristol-Coanda Monoplanes

TypeAircraft
Company

Bristol Aeroplane Company

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
8.9
88.7
Height (m)
0.6
 
2.1
50.1
Wings
Wing area (m2)
1.1
 
41.8
925
Wingspan (Beam) (m)
0.1
 
11.5
95
Weights
Empty weight (kg)
8
 
440.0
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
755.2
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
113
28,165
105 - 113 km/h
Сruise Speed (km/h)
52
 
82
3,087
Power
Total Power (hp)
0.4
 
100
60,000
1 powerplant
Performance
Endurance (h)
0.0
 
5
150
Dynamic Performance
Time to altitude (min)
0.6
 
11
105
to 915 m
Combat
Bombs (qt)
1
 
12
250
4.5 kg light bombs
Stat
Number built (qt)
0
 
37
43,000
Introduction 1912
First flight 1912

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