Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      10 m2
      16 m2
    • Wingspan (Beam)
      7 m
      11 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
      1116 kg
      1674 kg
    • Max. takeoff weight (Gross weight)
      1640 kg
      2460 kg
    • Loaded weight
      1400 kg
      2100 kg
    • Crew
      1 per.
      2 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
      389 km/h
      585 km/h
    • Сruise Speed
      380 km/h
      572 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
      400 hp
      600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3200 m
      4800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      720 km
      1080 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
      464 m/min
      696 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
      3 qt
      5 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
      72 qt
      108 qt
    • Price
      41 USD
      750000000 USD

Caudron C.710

TypeAircraft
Company

Société des avions Caudron

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
8.6
88.7
Height (m)
0.6
 
2.9
50.1
Wings
Wing area (m2)
1.1
 
12.5
925
Wingspan (Beam) (m)
0.1
 
9.0
95
Weights
Empty weight (kg)
8
 
1,395
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,050
575,000
Loaded weight (kg)
5
 
1,750
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
487
28,165
at 4000 m
Сruise Speed (km/h)
52
 
476
3,087
Power
Total Power (hp)
0.4
 
500
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,000
161,544
Range (Ferry range) (km)
4
 
900
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
580
36,000
Combat
Guns (qt)
1
 
4
18
7.5 mm MAC 1934 machine guns
Stat
Number built (qt)
0
 
90
43,000
Introduction 1940
First flight 18.07.1936
Stop production 1941

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