Search filter

    • Year
      1906
      2018
    • Length
      7 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      15 m2
      23 m2
    • Wingspan (Beam)
      9 m
      14 m
    • Wing loading
      124 kg/m2
      187 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      5
      9
    • Disc area
      1 m2
      460 m2
    • Main rotor diameter
      1 m
      62 m
    • Rotor number
      2 qt
      4 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
      1812 kg
      2718 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      2308 kg
      3462 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
      455 km/h
      683 km/h
    • Сruise Speed
      435 km/h
      653 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
      2 hp/kg
      5 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      1179 hp
      1769 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6400 m
      9600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      760 km
      1140 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
      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
      2 qt
      4 qt
    • Guns
      2 qt
      4 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Caproni Vizzola F.6

TypeAircraft
Company

Caproni

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
9.2
88.7
or 9,01 depending on variant
Height (m)
0.6
 
3.0
50.1
Wings
Wing area (m2)
1.1
 
18.8
925
Wingspan (Beam) (m)
0.1
 
11.4
95
or 11,82 m depending on variant
Wing loading (kg/m2)
3.1
 
155.4
829
Aspect ratio
1.7
 
6.9
25.6
Rotors
Rotor number (qt)
1
 
3
8
Weights
Empty weight (kg)
8
 
2,265
276,800
or 3348 kg depending on variant
Loaded weight (kg)
5
 
2,885
242,500
or 4092 kg depending on variant
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
569
28,165
(or 630 depending on variant) at 5000 m
Сruise Speed (km/h)
52
 
544
3,087
Power
Power/mass (hp/kg)
0.0
 
3.5
22.1
Total Power (hp)
0.4
 
1,474
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,000
161,544
Range (Ferry range) (km)
4
 
950
40,700
or 1370 depending on variant at 477 km/h
Propellers
Prop blade number (qt)
1
 
3
8
Combat
Guns (qt)
1
 
3
18
(or for depending on variant) 12.7 mm (0.5 in) forward-firing Breda-SAFAT machine guns
Stat
Number built (qt)
0
 
2
43,000
Introduction 1941
First flight 01.09.1941

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