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    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      41 m2
      62 m2
    • Wingspan (Beam)
      11 m
      17 m
    • Wing loading
      39 kg/m2
      60 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
      1192 kg
      1788 kg
    • Max. takeoff weight (Gross weight)
      2000 kg
      3000 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      854 kg
      1282 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
      171 km/h
      257 km/h
    • Сruise Speed
      140 km/h
      212 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
      382 hp
      575 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4400 m
      6600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      480 km
      720 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      400 km
      600 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
      168 m/min
      252 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
      3200 qt
      4800 qt
    • Price
      41 USD
      750000000 USD

Potez 25

TypeAircraft
Company

Potez

Scheme

Biplane

Geometry
Length (m)
1.9
 
9.2
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
51.4
925
Wingspan (Beam) (m)
0.1
 
14.1
95
Wing loading (kg/m2)
3.1
 
49.8
829
Weights
Empty weight (kg)
8
 
1,490
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,500
575,000
Capacity
Crew (per.)
1
 
2
112
Useful load (kg)
26.4
 
1,068
90,700
Speeds
Max. Speed (km/h)
25
 
214
28,165
Сruise Speed (km/h)
52
 
176
3,087
Power
Total Power (hp)
0.4
 
478.6
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,500
161,544
Range (Ferry range) (km)
4
 
600
40,700
Сombat radius (km)
277
 
500
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
210
36,000
Stat
Number built (qt)
0
 
4,000
43,000
4,000 (2,500 in France)
Introduction 1925
First flight 1924
Stop production 1940

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