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    • Year
      1906
      2018
    • Length
      19 m
      30 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      80 m2
      120 m2
    • Wingspan (Beam)
      20 m
      32 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
      7200 kg
      10800 kg
    • Max. takeoff weight (Gross weight)
      10864 kg
      16296 kg
    • Loaded weight
      10444 kg
      15666 kg
    • Crew
      3 per.
      5 per.
    • Useful load
      3664 kg
      5496 kg
    • Payload
      3664 kg
      5496 kg
    • Capacity passengers
      21 per.
      33 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      280 km/h
      420 km/h
    • Сruise Speed
      228 km/h
      342 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      80 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
      2196 hp
      3294 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6400 m
      9600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      800 km
      1200 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
      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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Bloch MB.300

TypeAircraft
Company

Société des Avions Marcel Bloch

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
24.9
88.7
Height (m)
0.6
 
6.8
50.1
Wings
Wing area (m2)
1.1
 
100
925
Wingspan (Beam) (m)
0.1
 
25.9
95
Weights
Empty weight (kg)
8
 
9,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
13,580
575,000
Loaded weight (kg)
5
 
13,055
242,500
Capacity
Crew (per.)
1
 
4
112
Useful load (kg)
26.4
 
4,580
90,700
Payload (kg)
23
 
4,580
122,470
Capacity passengers (per.)
1
 
27
400
or 12 passenger sleeper
Speeds
Max. Speed (km/h)
25
 
350
28,165
at 2200 m
Сruise Speed (km/h)
52
 
285
3,087
Minimum control speed (km/h)
24
 
100
113
Power
Total Power (hp)
0.4
 
2,745
60,000
3 powerplants 915 hp each
Performance
Service ceiling (m)
0.6
 
8,000
161,544
Range (Ferry range) (km)
4
 
1,000
40,700
Stat
Number built (qt)
0
 
1
43,000
Introduction 1935
First flight 1935

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