Search filter

    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      48 m2
      74 m2
    • Wingspan (Beam)
      16 m
      26 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
      7076 kg
      10616 kg
    • Max. takeoff weight (Gross weight)
      10630 kg
      15946 kg
    • Loaded weight
      5 kg
      242500 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
      345 km/h
      519 km/h
    • Сruise Speed
      276 km/h
      416 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
      2400 hp
      3600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6320 m
      9480 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1464 km
      2196 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
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      3 qt
    • Bombs weight
      1600 kg
      2400 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      263 qt
      395 qt
    • Price
      41 USD
      750000000 USD

SIAI Savoia-Marchetti SM.84

TypeAircraft
Company

SIAI-Marchetti

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
17.9
88.7
Height (m)
0.6
 
4.6
50.1
Wings
Wing area (m2)
1.1
 
61
925
Wingspan (Beam) (m)
0.1
 
21.1
95
Weights
Empty weight (kg)
8
 
8,846
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
13,288
575,000
Capacity
Crew (per.)
1
 
5
112
Speeds
Max. Speed (km/h)
25
 
432
28,165
Сruise Speed (km/h)
52
 
346
3,087
Power
Total Power (hp)
0.4
 
3,000
60,000
3 powerplants 1000 hp
Performance
Service ceiling (m)
0.6
 
7,900
161,544
Range (Ferry range) (km)
4
 
1,830
40,700
Combat
Guns (qt)
1
 
4
18
12.7 mm (.50 in) Scotti machine guns (1 in dorsal turret, 1 in ventral position and 2 in waist positions
Torpedoes (qt)
1
 
2
4
Bombs weight (kg)
2
 
2,000
39,000
Stat
Number built (qt)
0
 
329
43,000
Introduction 1941
First flight 05.06.1940
Stop production 1948

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