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    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      19 m2
      30 m2
    • Wingspan (Beam)
      10 m
      16 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
      883 kg
      1325 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1296 kg
      1944 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
      173 km/h
      261 km/h
    • Сruise Speed
      142 km/h
      214 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
      280 hp
      420 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4400 m
      6600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      400 km
      600 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      4 h
      7 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
      256 m/min
      384 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      5 min
      9 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      2 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
      12 qt
      20 qt
    • Price
      41 USD
      750000000 USD

Potez 452

TypeAircraft
Company

Potez

Scheme

Monoplane

Parasol

Geometry
Length (m)
1.9
 
10.2
88.7
Height (m)
0.6
 
3.4
50.1
Wings
Wing area (m2)
1.1
 
24.3
925
Wingspan (Beam) (m)
0.1
 
13
95
Weights
Empty weight (kg)
8
 
1,104
276,800
Loaded weight (kg)
5
 
1,620
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
217
28,165
at 2000 m
Сruise Speed (km/h)
52
 
178
3,087
Power
Total Power (hp)
0.4
 
350
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,500
161,544
Range (Ferry range) (km)
4
 
500
40,700
Endurance (h)
0.0
 
5.2
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
320
36,000
Time to altitude (min)
0.6
 
7.3
105
to 2000 m
Combat
Guns (qt)
1
 
1
18
7.5 mm (0.295 inch) machine gun mounted in flexible position in rear cockpit
Stat
Number built (qt)
0
 
16
43,000
Introduction 1936
First flight 1935
Stop production 1944

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