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    • Year
      1906
      2018
    • Length
      15 m
      23 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      18 m
      28 m
    • Wing loading
      124 kg/m2
      188 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
      5130 kg
      7696 kg
    • Max. takeoff weight (Gross weight)
      8176 kg
      12266 kg
    • Loaded weight
      7792 kg
      11688 kg
    • Crew
      4 per.
      6 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
      257 km/h
      387 km/h
    • Сruise Speed
      192 km/h
      288 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
      7920 m
      11880 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1360 km
      2040 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
      9 min
      15 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
      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
      240 qt
      360 qt
    • Price
      41 USD
      750000000 USD

Bloch MB.210

TypeAircraft
Company

Société des Avions Marcel Bloch

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
18.8
88.7
Height (m)
0.6
 
6.7
50.1
Wings
Wingspan (Beam) (m)
0.1
 
22.8
95
Wing loading (kg/m2)
3.1
 
156
829
Weights
Empty weight (kg)
8
 
6,413
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
10,221
575,000
Loaded weight (kg)
5
 
9,740
242,500
Capacity
Crew (per.)
1
 
5
112
Speeds
Max. Speed (km/h)
25
 
322
28,165
at 3500 m
Сruise Speed (km/h)
52
 
240
3,087
at 3500 econ cruise
Power
Total Power (hp)
0.4
 
1,900
60,000
2 powerplants
Performance
Service ceiling (m)
0.6
 
9,900
161,544
Range (Ferry range) (km)
4
 
1,700
40,700
Dynamic Performance
Time to altitude (min)
0.6
 
12
105
to 4000 m
Combat
Guns (qt)
1
 
3
18
7.5 mm (.295 in) MAC 1934 machine guns (one in nose, dorsal and vental turrets)
Stat
Number built (qt)
0
 
300
43,000
Introduction 01.11.1936
First flight 23.11.1934
Stop production 1945

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