Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      48 m2
      72 m2
    • Wingspan (Beam)
      15 m
      23 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
      4840 kg
      7262 kg
    • Max. takeoff weight (Gross weight)
      7640 kg
      11460 kg
    • Loaded weight
      7638 kg
      11458 kg
    • Crew
      4 per.
      6 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
      292 km/h
      438 km/h
    • Сruise Speed
      279 km/h
      420 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
      1600 hp
      2400 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5200 m
      7800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      959 km
      1439 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
      276 m/min
      414 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      13 min
      21 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
      1179 kg
      1769 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      112 qt
      168 qt
    • Price
      41 USD
      750000000 USD

Caproni Ca.135

TypeAircraft
Company

Caproni

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
14.4
88.7
Height (m)
0.6
 
3.4
50.1
Wings
Wing area (m2)
1.1
 
60
925
Wingspan (Beam) (m)
0.1
 
18.8
95
Weights
Empty weight (kg)
8
 
6,050.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
9,550
575,000
Loaded weight (kg)
5
 
9,548.1
242,500
Capacity
Crew (per.)
1
 
5
112
4-5
Speeds
Max. Speed (km/h)
25
 
365
28,165
at 4800 m
Сruise Speed (km/h)
52
 
349.2
3,087
Power
Total Power (hp)
0.4
 
2,000
60,000
2 powerplants 1000 hp each
Performance
Service ceiling (m)
0.6
 
6,500
161,544
Range (Ferry range) (km)
4
 
1,199
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
345
36,000
Time to altitude (min)
0.6
 
17.4
105
to 4999 m
Combat
Guns (qt)
1
 
3
18
12.7 mm (0.500 in) Breda-SAFAT machine guns
Bombs weight (kg)
2
 
1,474
39,000
Stat
Number built (qt)
0
 
140
43,000
approx. 140
Introduction 1935
First flight 01.04.1935

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