Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      36 m2
      56 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      33 kg/m2
      51 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
      912 kg
      1369 kg
    • Max. takeoff weight (Gross weight)
      1536 kg
      2306 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
      167 km/h
      251 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      139 km/h
      209 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
      340 hp
      510 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5364 m
      8047 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
      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
      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
      3 qt
    • Bombs
      3 qt
      5 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
      3 qt
      5 qt
    • Price
      41 USD
      750000000 USD

Bristol Type 84 Bloodhound

TypeAircraft
Company

Bristol Aeroplane Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
8.1
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wing area (m2)
1.1
 
45.9
925
Wingspan (Beam) (m)
0.1
 
12.3
95
Wing loading (kg/m2)
3.1
 
41.9
829
Weights
Empty weight (kg)
8
 
1,140.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,921
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Ground Speed (km/h)
96.6
 
209
1,500
Сruise Speed (km/h)
52
 
174
3,087
Power
Total Power (hp)
0.4
 
425
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,705.6
161,544
Combat
Guns (qt)
1
 
2
18
1 × fixed, forward-firing .303 in (7.7 mm) Vickers machine gun and 1 × .303 in (7.7 mm) Lewis gun on a Scarff ring in rear cockpit
Bombs (qt)
1
 
4
250
9 kg bombs
Stat
Number built (qt)
0
 
4
43,000
Introduction 1923
First flight 01.05.1923

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