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    • Year
      1906
      2018
    • Length
      8 m
      12 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      28 m2
      42 m2
    • Wingspan (Beam)
      12 m
      20 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
      1193 kg
      1791 kg
    • Max. takeoff weight (Gross weight)
      1811 kg
      2717 kg
    • Loaded weight
      1800 kg
      2700 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
      192 km/h
      288 km/h
    • Сruise Speed
      149 km/h
      225 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
      464 hp
      696 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5600 m
      8400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      640 km
      960 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
      7 min
      11 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
      96 kg
      144 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      89 qt
      135 qt
    • Price
      41 USD
      750000000 USD

Potez 39

TypeAircraft
Company

Potez

Scheme

Monoplane

Parasol

Geometry
Length (m)
1.9
 
10
88.7
Height (m)
0.6
 
3.4
50.1
Wings
Wing area (m2)
1.1
 
35
925
Wingspan (Beam) (m)
0.1
 
16
95
Weights
Empty weight (kg)
8
 
1,492
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,264
575,000
Loaded weight (kg)
5
 
2,250
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
240
28,165
at 3500 m
Сruise Speed (km/h)
52
 
187
3,087
Power
Total Power (hp)
0.4
 
580
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
7,000
161,544
Range (Ferry range) (km)
4
 
800
40,700
Dynamic Performance
Time to altitude (min)
0.6
 
9
105
to 3500 m
Combat
Guns (qt)
1
 
3
18
1 x 7.7 mm machine-gun firing forward, fixed; 2 x 7.7 mm machine-guns in observer's position, flexible
Bombs weight (kg)
2
 
120
39,000
Stat
Number built (qt)
0
 
112
43,000
Introduction 1930
First flight 1930
Stop production 1940

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