Search filter

    • Year
      1906
      2018
    • Length
      12 m
      20 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      48 m2
      72 m2
    • Wingspan (Beam)
      16 m
      26 m
    • Wing loading
      135 kg/m2
      203 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
      5440 kg
      8160 kg
    • Max. takeoff weight (Gross weight)
      8240 kg
      12360 kg
    • Loaded weight
      8240 kg
      12360 kg
    • Crew
      3 per.
      5 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      8 per.
      12 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      355 km/h
      533 km/h
    • Сruise Speed
      320 km/h
      480 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
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      1800 hp
      2700 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4400 m
      6600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1200 km
      1800 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      3 h
      5 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
      10 min
      17 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      18 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
      18 qt
      28 qt
    • Price
      41 USD
      750000000 USD

SIAI Savoia-Marchetti SM.83

TypeAircraft
Company

SIAI-Marchetti

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
16.2
88.7
Height (m)
0.6
 
4.1
50.1
Wings
Wing area (m2)
1.1
 
60
925
Wingspan (Beam) (m)
0.1
 
21.2
95
Wing loading (kg/m2)
3.1
 
169
829
Weights
Empty weight (kg)
8
 
6,800
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
10,300
575,000
Loaded weight (kg)
5
 
10,300
242,500
Capacity
Crew (per.)
1
 
4
112
3-4
Capacity passengers (per.)
1
 
10
400
Speeds
Max. Speed (km/h)
25
 
444
28,165
at 4000 m
Сruise Speed (km/h)
52
 
400
3,087
at 500 m with 70% power
Power
Power/mass (hp/kg)
0.0
 
0.2
22.1
Total Power (hp)
0.4
 
2,250
60,000
3 powerplants 750 hp each
Performance
Service ceiling (m)
0.6
 
8,400
161,544
0.6
 
5,500
161,544
with one engine stopped
Range (Ferry range) (km)
4
 
1,500
40,700
Endurance (h)
0.0
 
4
150
Dynamic Performance
Time to altitude (min)
0.6
 
9
105
to 3000 m
0.6
 
13.5
105
to 4000 m
Stat
Number built (qt)
0
 
23
43,000
Introduction 1938
First flight 19.11.1937
Stop production 1945

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