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    • Year
      1906
      2018
    • Length
      11 m
      17 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      53 m2
      81 m2
    • Wingspan (Beam)
      17 m
      27 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
      3 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
      9288 kg
      13934 kg
    • Max. takeoff weight (Gross weight)
      14152 kg
      21229 kg
    • Loaded weight
      5 kg
      242500 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
      460 km/h
      692 km/h
    • Сruise Speed
      400 km/h
      601 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
      3952 hp
      5928 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6340 m
      9510 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3604 km
      5408 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
      365 m/min
      549 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
      3 m
      6 m
    • Prop blade number
      3 qt
      5 qt
    • Guns
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      6 qt
      10 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      728 kg
      1092 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      117 qt
      177 qt
    • Price
      41 USD
      750000000 USD

Bristol Type 164 Brigand

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
 
66.7
925
Wingspan (Beam) (m)
0.1
 
22.1
95
Rotors
Rotor number (qt)
1
 
2
8
Weights
Empty weight (kg)
8
 
11,611.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
17,690.1
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
576.2
28,165
at 4900 m
Сruise Speed (km/h)
52
 
500.5
3,087
at 7000 m
Power
Total Power (hp)
0.4
 
4,940
60,000
2 powerlants 2470 hp each
Performance
Service ceiling (m)
0.6
 
7,925
161,544
Range (Ferry range) (km)
4
 
4,506
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
457.2
36,000
Propellers
Prop diameter (m)
1.8
 
4.3
5.8
Prop blade number (qt)
1
 
4
8
Combat
Guns (qt)
1
 
4
18
20 mm Hispano Mk V cannon
Rockets (qt)
1
 
8
76
RP-3 60 lb (27 kg) rockets
Bombs weight (kg)
2
 
910
39,000
under wings and fuselage
Stat
Number built (qt)
0
 
147
43,000
Introduction 1944
First flight 04.12.1944
Stop production 1958

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