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    • 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
      17 m2
      26 m2
    • Wingspan (Beam)
      6 m
      11 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
      597 kg
      897 kg
    • Max. takeoff weight (Gross weight)
      789 kg
      1185 kg
    • Loaded weight
      789 kg
      1185 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
      200 km/h
      300 km/h
    • Сruise Speed
      169 km/h
      255 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
      0 m
      161544 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
      1 h
      3 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
      400 m/min
      600 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      8 min
      14 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      3 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
      2 qt
      4 qt
    • Price
      41 USD
      750000000 USD

SIAI S.50

TypeAircraft
Company

SIAI-Marchetti

Scheme

Biplane

Geometry
Length (m)
1.9
 
7.8
88.7
Height (m)
0.6
 
2.6
50.1
Wings
Wing area (m2)
1.1
 
21.5
925
Wingspan (Beam) (m)
0.1
 
8.7
95
Weights
Empty weight (kg)
8
 
747
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
987
575,000
Loaded weight (kg)
5
 
987
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
250
28,165
Сruise Speed (km/h)
52
 
212
3,087
Power
Total Power (hp)
0.4
 
220
60,000
1 powerplant
Performance
Endurance (h)
0.0
 
2.1
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
500
36,000
Time to altitude (min)
0.6
 
2
105
to 1000 m
0.6
 
11
105
to 5000 m
Combat
Guns (qt)
1
 
2
18
fixed forward-firing synchronized 7.7-millimeter (0.303-inch) Vickers machine guns
Stat
Number built (qt)
0
 
3
43,000
Introduction 1922
First flight 1919

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