Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      7 m2
      11 m2
    • Wingspan (Beam)
      6 m
      10 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
      537 kg
      807 kg
    • Max. takeoff weight (Gross weight)
      840 kg
      1260 kg
    • Loaded weight
      840 kg
      1260 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
      296 km/h
      444 km/h
    • Сruise Speed
      272 km/h
      408 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
      176 hp
      264 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7760 m
      11640 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      880 km
      1320 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
      528 m/min
      792 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
      15 qt
      23 qt
    • Price
      41 USD
      750000000 USD

Caudron C.690

TypeAircraft
Company

Société des avions Caudron

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
7.8
88.7
Height (m)
0.6
 
2.6
50.1
Wings
Wing area (m2)
1.1
 
9
925
Wingspan (Beam) (m)
0.1
 
7.7
95
Weights
Empty weight (kg)
8
 
672
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,050
575,000
Loaded weight (kg)
5
 
1,050
242,500
Capacity
Crew (per.)
1
 
1
112
pilot
Speeds
Max. Speed (km/h)
25
 
370
28,165
Сruise Speed (km/h)
52
 
340
3,087
Power
Total Power (hp)
0.4
 
220
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
9,700
161,544
Range (Ferry range) (km)
4
 
1,100
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
660
36,000
Stat
Number built (qt)
0
 
19
43,000
Introduction 1936
First flight 18.02.1936

Similar aircraft

Get more

Comments