Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      30 m2
      46 m2
    • Wingspan (Beam)
      14 m
      22 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
      4489 kg
      6735 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      5728 kg
      8592 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
      424 km/h
      636 km/h
    • Сruise Speed
      368 km/h
      552 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
      1656 hp
      2484 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8800 m
      13200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1320 km
      1980 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1032 km
      1548 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
      8 min
      14 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      5 qt
      9 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Bloch MB.170

TypeAircraft
Company

Société des Avions Marcel Bloch

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
12.2
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
38
925
Wingspan (Beam) (m)
0.1
 
17.9
95
Weights
Empty weight (kg)
8
 
5,612
276,800
Loaded weight (kg)
5
 
7,160
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
530
28,165
at 5200 m
Сruise Speed (km/h)
52
 
460
3,087
at 4000 m
Power
Total Power (hp)
0.4
 
2,070
60,000
2 powerplants 1035 hp each
Performance
Service ceiling (m)
0.6
 
11,000
161,544
Range (Ferry range) (km)
4
 
1,650
40,700
Сombat radius (km)
277
 
1,290
7,210
Dynamic Performance
Time to altitude (min)
0.6
 
11
105
to 8000 m
Combat
Guns (qt)
1
 
7
18
2 × fixed, forward-firing 7.5 mm (.295 in) MAC 1934 machine guns in the wings; 2 × 7.5 mm (.295 in) MAC 1934s in the dorsal position; 3 × 7.5 mm (.295 in) MAC 1934s on aft-firing mounts
Bombs (qt)
1
 
8
250
50 kg bombs
Stat
Introduction 01.03.1940
First flight 01.07.1939
Stop production 1950

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