Search filter

    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      0 m
      95 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
      11 m
      18 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
      2837 kg
      4257 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      3992 kg
      5988 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      10 per.
      16 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      109 km/h
      165 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
      880 hp
      1320 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4780 m
      7170 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      238 km
      358 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
      288 m/min
      432 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
      4 qt
      6 qt
    • Price
      41 USD
      750000000 USD

Bristol Type 173

TypeHelicopter
Company

Bristol Aeroplane Company

Geometry
Length (m)
1.9
 
16.8
88.7
Height (m)
0.6
 
4.6
50.1
Rotors
Main rotor diameter (m)
1.2
 
14.8
62
Weights
Empty weight (kg)
8
 
3,547
276,800
Loaded weight (kg)
5
 
4,990
242,500
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
13
400
Speeds
Сruise Speed (km/h)
52
 
137
3,087
Power
Total Power (hp)
0.4
 
1,100
60,000
2 powerplants 550 hp each
Performance
Service ceiling (m)
0.6
 
5,975
161,544
Range (Ferry range) (km)
4
 
298
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
360
36,000
Stat
Number built (qt)
0
 
5
43,000
Introduction 1952
First flight 03.01.1952

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