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    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      26 m2
      40 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
      2508 kg
      3762 kg
    • Max. takeoff weight (Gross weight)
      3624 kg
      5436 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 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
      296 km/h
      444 km/h
    • Max. Speed
      340 km/h
      510 km/h
    • Сruise Speed
      240 km/h
      360 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
      760 l
      1140 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
      1120 hp
      1680 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6800 m
      10200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1200 km
      1800 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
      403 m/min
      605 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
      2 qt
      4 qt
    • Bombs
      3 qt
      5 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
      43000 qt
    • Price
      41 USD
      750000000 USD

Potez 630

TypeAircraft
Company

Potez

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
10.9
88.7
Height (m)
0.6
 
3.1
50.1
Wings
Wing area (m2)
1.1
 
32.7
925
Wingspan (Beam) (m)
0.1
 
16
95
Weights
Empty weight (kg)
8
 
3,135
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,530
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Ground Speed (km/h)
96.6
 
370
1,500
Max. Speed (km/h)
25
 
425
28,165
at 5000 m
Сruise Speed (km/h)
52
 
300
3,087
at 4500 m
Fuel
Fuel Capacity (l)
23
 
950
320,000
Power
Total Power (hp)
0.4
 
1,400
60,000
2 powerplants 700 hp each
Performance
Service ceiling (m)
0.6
 
8,500
161,544
Range (Ferry range) (km)
4
 
1,500
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
504
36,000
Combat
Guns (qt)
1
 
3
18
1x fixed, forward-firing 7.5 mm MAC 1934 machine gun; 1x fixed, rearward-firing 7.5 mm MAC 1934 machine gun; 1x flexibly mounted, rearward-firing 7.5 mm MAC 1934 machine gun
Bombs (qt)
1
 
4
250
50 kg (110 lb) bombs
Stat
Introduction 1938
First flight 25.04.1936
Stop production 1942

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