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    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      34 m2
      52 m2
    • Wingspan (Beam)
      10 m
      17 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
      1052 kg
      1579 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1621 kg
      2433 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
      173 km/h
      261 km/h
    • Сruise Speed
      145 km/h
      219 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
      8 min
      13 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
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      3 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      3 qt
      5 qt
    • Price
      41 USD
      750000000 USD

Bristol Type 93 Boarhound

TypeAircraft
Company

Bristol Aeroplane Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
9.6
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
43.1
925
Wingspan (Beam) (m)
0.1
 
13.6
95
Weights
Empty weight (kg)
8
 
1,315.4
276,800
Loaded weight (kg)
5
 
2,027
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and observer
Speeds
Max. Speed (km/h)
25
 
217
28,165
Сruise Speed (km/h)
52
 
182
3,087
Power
Total Power (hp)
0.4
 
425
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,705.6
161,544
Dynamic Performance
Time to altitude (min)
0.6
 
10.6
105
to 3050 m
Combat
Guns (qt)
1
 
2
18
1 × forward-firing .303 in (7.7 mm) Vickers machine gun on side of fuselage; 1 × .303 in (7.7 mm) Lewis Gun on Scarff ring (observer)
Bombs weight (kg)
2
 
2
39,000
50 kg bombs
Stat
Number built (qt)
0
 
4
43,000
Introduction 1928
First flight 08.06.1925

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