Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      56 m2
      84 m2
    • Wingspan (Beam)
      16 m
      26 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
      1368 kg
      2052 kg
    • Max. takeoff weight (Gross weight)
      1320 kg
      1980 kg
    • Loaded weight
      1864 kg
      2796 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
      96 km/h
      1500 km/h
    • Max. Speed
      108 km/h
      164 km/h
    • Сruise Speed
      92 km/h
      138 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
      208 hp
      312 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3680 m
      5520 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
      2 h
      4 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
      91 m/min
      137 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
      80 kg
      120 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      199 qt
      299 qt
    • Price
      41 USD
      750000000 USD

Caudron R.4

TypeAircraft
Company

Société des avions Caudron

Scheme

Biplane

Geometry
Length (m)
1.9
 
11.8
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
70
925
Wingspan (Beam) (m)
0.1
 
21.1
95
Weights
Empty weight (kg)
8
 
1,710
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,650
575,000
Loaded weight (kg)
5
 
2,330
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
136
28,165
Сruise Speed (km/h)
52
 
115
3,087
Power
Total Power (hp)
0.4
 
260
60,000
2 powerplants 130 hp each
Performance
Service ceiling (m)
0.6
 
4,600
161,544
Endurance (h)
0.0
 
3
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
114
36,000
Combat
Guns (qt)
1
 
4
18
.303 Lewis guns
Bombs weight (kg)
2
 
100
39,000
Stat
Number built (qt)
0
 
249
43,000
Introduction 1915

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