Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      0 m
      51 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      52 m2
      78 m2
    • Wingspan (Beam)
      16 m
      24 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
      1968 kg
      2952 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      3200 kg
      4800 kg
    • Crew
      1 per.
      112 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      7 per.
      11 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      180 km/h
      270 km/h
    • Max. Speed
      25 km/h
      28165 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
      488 l
      733 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
      480 hp
      720 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4160 m
      6240 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      14 min
      22 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      3 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

Potez 38

Company

Potez

Scheme

Monoplane

Geometry
Length (m)
1.9
 
14.8
88.7
Wings
Wing area (m2)
1.1
 
65
925
Wingspan (Beam) (m)
0.1
 
20
95
Weights
Empty weight (kg)
8
 
2,460
276,800
equipped
Loaded weight (kg)
5
 
4,000
242,500
Capacity
Capacity passengers (per.)
1
 
9
400
Speeds
Ground Speed (km/h)
96.6
 
225
1,500
Fuel
Fuel Capacity (l)
23
 
610.3
320,000
Power
Total Power (hp)
0.4
 
600
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,200
161,544
Dynamic Performance
Time to altitude (min)
0.6
 
18
105
to 3000 m
Propellers
Propellers (qt)
1
 
1
8
Prop blade number (qt)
1
 
2
8
Stat
Number built (qt)
0
 
1
43,000
First flight 1930

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