Search filter

    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      16 m
      25 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
      3752 kg
      5628 kg
    • Max. takeoff weight (Gross weight)
      6880 kg
      10320 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 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
      279 km/h
      419 km/h
    • Сruise Speed
      224 km/h
      336 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
      1520 hp
      2280 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5800 m
      8700 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1040 km
      1560 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
      10 min
      16 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      2 qt
      4 qt
    • Bombs
      51 qt
      77 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
      114 qt
      172 qt
    • Price
      41 USD
      750000000 USD

Bloch MB.131

TypeAircraft
Company

Société des Avions Marcel Bloch

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
17.9
88.7
Height (m)
0.6
 
4.1
50.1
Wings
Wingspan (Beam) (m)
0.1
 
20.3
95
Weights
Empty weight (kg)
8
 
4,690
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,600
575,000
Capacity
Crew (per.)
1
 
4
112
Speeds
Max. Speed (km/h)
25
 
349
28,165
at 3750 m
Сruise Speed (km/h)
52
 
280
3,087
Power
Total Power (hp)
0.4
 
1,900
60,000
2 powerplants 950 hp each
Performance
Service ceiling (m)
0.6
 
7,250
161,544
Range (Ferry range) (km)
4
 
1,300
40,700
Dynamic Performance
Time to altitude (min)
0.6
 
13
105
to 4000 m
Combat
Guns (qt)
1
 
3
18
7.5 mm (.295 in) MAC 1934 machine guns in flexible mounts in the nose, dorsal turret, and ventral gondola
Bombs (qt)
1
 
4
250
200 kg bombs or
1
 
6
250
100 kg bombs or
1
 
8
250
50 kg bombs or
1
 
64
250
10 kg bombs
Stat
Number built (qt)
0
 
143
43,000
Introduction 1934
First flight 29.06.1934

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