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    • Year
      1906
      2018
    • Length
      16 m
      26 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      99 m2
      150 m2
    • Wingspan (Beam)
      23 m
      36 m
    • Wing loading
      58 kg/m2
      88 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
      5007 kg
      7512 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      7338 kg
      11008 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
      247 km/h
      371 km/h
    • Сruise Speed
      214 km/h
      322 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
      1616 hp
      2424 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6059 m
      9090 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2874 km
      4312 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
      182 m/min
      275 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
      6 qt
      10 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
      40 qt
      62 qt
    • Price
      41 USD
      750000000 USD

Bristol Type 130 Bombay

TypeAircraft
Company

Bristol Aeroplane Company

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
21.1
88.7
Height (m)
0.6
 
6.1
50.1
Wings
Wing area (m2)
1.1
 
124.7
925
Wingspan (Beam) (m)
0.1
 
29.2
95
Wing loading (kg/m2)
3.1
 
72.9
829
Weights
Empty weight (kg)
8
 
6,259.6
276,800
Loaded weight (kg)
5
 
9,173
242,500
Capacity
Crew (per.)
1
 
3
112
3-4
Speeds
Max. Speed (km/h)
25
 
309
28,165
at 2000 m
Сruise Speed (km/h)
52
 
268
3,087
at 3050 m
Power
Total Power (hp)
0.4
 
2,020
60,000
2 powerplants 1010 hp each
Performance
Service ceiling (m)
0.6
 
7,574.3
161,544
Range (Ferry range) (km)
4
 
3,592.9
40,700
with overload fuel
Dynamic Performance
Rate of climb (m/min)
1.9
 
228.6
36,000
Combat
Guns (qt)
1
 
2
18
0.303 in (7.7 mm) Vickers K machine guns in powered nose and tail turrets
Bombs (qt)
1
 
8
250
113 kg bombs on underfuselage racks
Stat
Number built (qt)
0
 
51
43,000
Introduction 1935
First flight 23.06.1935
Stop production 1944

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