Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      13 m
      21 m
    • Wing loading
      120 kg/m2
      180 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
      3552 kg
      5329 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      5236 kg
      7854 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
      342 km/h
      514 km/h
    • Сruise Speed
      52 km/h
      3087 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
      1472 hp
      2208 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6647 m
      9971 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1880 km
      2822 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
      1 m
      3 m
    • Prop blade number
      2 qt
      4 qt
    • Guns
      4 qt
      6 qt
    • Bombs
      8 qt
      12 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
      3537 qt
      5307 qt
    • Price
      41 USD
      750000000 USD

Bristol Type 142M Blenheim

TypeAircraft
Company

Bristol Aeroplane Company

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
13.0
88.7
Height (m)
0.6
 
3
50.1
Wings
Wingspan (Beam) (m)
0.1
 
17.2
95
Wing loading (kg/m2)
3.1
 
150
829
Weights
Empty weight (kg)
8
 
4,440.7
276,800
Loaded weight (kg)
5
 
6,545
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
428
28,165
at 3597
Power
Total Power (hp)
0.4
 
1,840
60,000
2 powerplants 920 hp each
Performance
Service ceiling (m)
0.6
 
8,308.9
161,544
Range (Ferry range) (km)
4
 
2,351
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
457.2
36,000
Propellers
Prop diameter (m)
1.8
 
2
5.8
Prop blade number (qt)
1
 
3
8
per propeller
Combat
Guns (qt)
1
 
4
18
1 × .303 in (7.7 mm) Browning machine gun in port wing; 1 × .303 in (7.7 mm) Browning guns in rear-firing under-nose blister or Nash & Thomson FN.54 turret; 2 × .303 in (7.7 mm) Browning guns in dorsal turret or
1
 
5
18
1 × .303 in (7.7 mm) Browning machine gun in port wing; 2 × .303 in (7.7 mm) Browning guns in rear-firing under-nose blister and Nash & Thomson FN.54 turret; 2 × .303 in (7.7 mm) Browning guns in dorsal turret
Bombs (qt)
1
 
12
250
8 x 113 kg bombs and 8× 40 lb (18 kg) bombs externally or
1
 
10
250
2 x 227 kg bombs internally and 8× 40 lb (18 kg) bombs externally
Stat
Number built (qt)
0
 
4,422
43,000
Introduction 1937
First flight 12.04.1935
Stop production 1944

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