Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 m2
    • Wingspan (Beam)
      12 m
      20 m
    • Wing loading
      15 kg/m2
      23 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      9
      14
    • 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
      192 kg
      288 kg
    • Max. takeoff weight (Gross weight)
      352 kg
      528 kg
    • Loaded weight
      336 kg
      504 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
      84 km/h
      126 km/h
    • Сruise Speed
      52 km/h
      3087 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
      136 km/h
      204 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
      0 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4240 m
      6360 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      44 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
      252 qt
      378 qt
    • Price
      41 USD
      750000000 USD

Caudron C.800

TypeGlider
Company

Société des avions Caudron

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
8.4
88.7
Height (m)
0.6
 
2.4
50.1
Wings
Wing area (m2)
1.1
 
22
925
Wingspan (Beam) (m)
0.1
 
16
95
Wing loading (kg/m2)
3.1
 
19.1
829
Aspect ratio
1.7
 
11.6
25.6
Weights
Empty weight (kg)
8
 
240
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
440
575,000
Loaded weight (kg)
5
 
420
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
105
28,165
Never exceed speed (km/h)
108.0
 
170
1,050
Performance
Service ceiling (m)
0.6
 
5,300
161,544
Dynamic Performance
Rate of sink (m/min)
36
 
55.8
55.8
Stat
Number built (qt)
0
 
315
43,000
Introduction 1942
First flight 01.04.1942

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