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    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      52 m2
      79 m2
    • Wingspan (Beam)
      17 m
      27 m
    • Wing loading
      185 kg/m2
      279 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
      8724 kg
      13087 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      12224 kg
      18336 kg
    • Crew
      2 per.
      4 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
      452 km/h
      680 km/h
    • Сruise Speed
      424 km/h
      636 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
      4136 hp
      6204 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7315 m
      10973 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2560 km
      3840 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
      547 m/min
      822 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
      89 qt
      135 qt
    • Price
      41 USD
      750000000 USD

Bristol Type 166 Buckmaster

TypeAircraft
Company

Bristol Aeroplane Company

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
14.2
88.7
Height (m)
0.6
 
5.3
50.1
Wings
Wing area (m2)
1.1
 
65.8
925
Wingspan (Beam) (m)
0.1
 
21.9
95
Wing loading (kg/m2)
3.1
 
232
829
Weights
Empty weight (kg)
8
 
10,905.3
276,800
Loaded weight (kg)
5
 
15,280
242,500
Capacity
Crew (per.)
1
 
3
112
student pilot, instructor pilot, radio operator
Speeds
Max. Speed (km/h)
25
 
566
28,165
at 3700 m
Сruise Speed (km/h)
52
 
530
3,087
at 5500 m
Power
Total Power (hp)
0.4
 
5,170
60,000
2 powerplants 2585 hp each
Performance
Service ceiling (m)
0.6
 
9,144
161,544
Range (Ferry range) (km)
4
 
3,200
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
684.3
36,000
Stat
Number built (qt)
0
 
112
43,000
Introduction 1944
First flight 27.10.1944

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