Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      132 kg/m2
      198 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
      1720 kg
      2580 kg
    • Max. takeoff weight (Gross weight)
      2560 kg
      3840 kg
    • Loaded weight
      2280 kg
      3420 kg
    • Crew
      1 per.
      3 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
      572 km/h
      858 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
      568 l
      852 l
    • Fuel External
      142 l
      209 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      6 kN
      10 kN
    • Service ceiling
      8800 m
      13200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      740 km
      1110 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
      13 m/min
      21 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
      3 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      112 kg
      168 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      743 qt
      1115 qt
    • Price
      60000 USD
      90000 USD

Fouga CM.170

TypeAircraft
Company

Fouga

Potez

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
10.1
88.7
Height (m)
0.6
 
2.1
50.1
Wings
Wingspan (Beam) (m)
0.1
 
12.2
95
Wing loading (kg/m2)
3.1
 
165
829
Weights
Empty weight (kg)
8
 
2,150
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,200
575,000
Loaded weight (kg)
5
 
2,850
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
715
28,165
Fuel
Fuel Capacity (l)
23
 
710
320,000
Fuel External (l)
142.5
 
173.8
10,025
Power
Thrust/weight (kN/kg)
0.0
 
0.3
2.1
Thrust (kN)
1.5
 
7.8
1,914
2 powerplants 3,92 kN each
Performance
Service ceiling (m)
0.6
 
11,000
161,544
Range (Ferry range) (km)
4
 
925
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
17
36,000
Combat
Guns (qt)
1
 
2
18
7.5 mm or 7.62 mm machine guns
Bombs weight (kg)
2
 
140
39,000
Stat
Number built (qt)
0
 
929
43,000
Price (USD)
41.5
 
75,000
750.0 million
Introduction 1978
First flight 23.07.1952

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