Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      48 m2
      72 m2
    • Wingspan (Beam)
      12 m
      19 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
      1560 kg
      2340 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      2360 kg
      3540 kg
    • Crew
      1 per.
      3 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
      152 km/h
      228 km/h
    • Сruise Speed
      52 km/h
      3087 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
      408 hp
      612 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3640 m
      5460 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3840 km
      5760 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      4 h
      6 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
      17 m/min
      27 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
      1 qt
      2 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      224 kg
      336 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      192 qt
      288 qt
    • Price
      41 USD
      750000000 USD

SIAI Savoia-Marchetti S.59

Company

SIAI-Marchetti

Scheme

Biplane

Geometry
Length (m)
1.9
 
10.4
88.7
Height (m)
0.6
 
3.5
50.1
Wings
Wing area (m2)
1.1
 
60
925
Wingspan (Beam) (m)
0.1
 
15.5
95
Weights
Empty weight (kg)
8
 
1,950
276,800
Loaded weight (kg)
5
 
2,950
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
190
28,165
Power
Total Power (hp)
0.4
 
510
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,550
161,544
Range (Ferry range) (km)
4
 
4,800
40,700
Endurance (h)
0.0
 
5
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
22
36,000
to 3000 m
Combat
Guns (qt)
1
 
1
18
7.7 mm (0.303 in) Lewis Gun
Bombs weight (kg)
2
 
280
39,000
of bombs on external racks
Stat
Number built (qt)
0
 
240
43,000
First flight 1925

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