Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      30 m2
      47 m2
    • Wingspan (Beam)
      12 m
      20 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
      1568 kg
      2352 kg
    • Max. takeoff weight (Gross weight)
      2344 kg
      3516 kg
    • Loaded weight
      5 kg
      242500 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
      200 km/h
      300 km/h
    • Сruise Speed
      168 km/h
      252 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
      624 hp
      936 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3400 m
      5100 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      840 km
      1260 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
      1 qt
      8 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
      264 kg
      396 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Caproni Ca.309 Ghibli

TypeAircraft
Company

Caproni

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
12.9
88.7
Height (m)
0.6
 
3.0
50.1
Wings
Wing area (m2)
1.1
 
38.7
925
Wingspan (Beam) (m)
0.1
 
16.2
95
Weights
Empty weight (kg)
8
 
1,960
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,930
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
250
28,165
Сruise Speed (km/h)
52
 
210
3,087
Power
Total Power (hp)
0.4
 
780
60,000
2 powerplants 390 hp each
Performance
Service ceiling (m)
0.6
 
4,250
161,544
Range (Ferry range) (km)
4
 
1,050
40,700
Combat
Guns (qt)
1
 
3
18
7.7 mm (.303 in) Breda SAFAT machine guns
Bombs weight (kg)
2
 
330
39,000
Stat
Introduction 1936
First flight 1937
Stop production 1948

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