Search filter

    • Year
      1906
      2018
    • Length
      10 m
      17 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      30 m2
      47 m2
    • Wingspan (Beam)
      14 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
      4720 kg
      7080 kg
    • Max. takeoff weight (Gross weight)
      7000 kg
      10500 kg
    • Loaded weight
      5 kg
      242500 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
      492 km/h
      738 km/h
    • Сruise Speed
      432 km/h
      648 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
      2000 hp
      3000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9600 m
      14400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1600 km
      2400 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
      672 m/min
      1008 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      5 min
      9 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      4 qt
      8 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      1600 kg
      2400 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

SIAI Savoia-Marchetti SM.92

TypeAircraft
Company

SIAI-Marchetti

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
13.7
88.7
Height (m)
0.6
 
4.2
50.1
Wings
Wing area (m2)
1.1
 
38.5
925
Wingspan (Beam) (m)
0.1
 
18.6
95
Weights
Empty weight (kg)
8
 
5,900
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,750
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
615
28,165
Сruise Speed (km/h)
52
 
540
3,087
Power
Total Power (hp)
0.4
 
2,500
60,000
2 powerplants 1250 hp each
Performance
Service ceiling (m)
0.6
 
12,000
161,544
Range (Ferry range) (km)
4
 
2,000
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
840
36,000
Time to altitude (min)
0.6
 
7.2
105
to 6000 m
Combat
Guns (qt)
1
 
6
18
3 × 20 mm MG 151 cannons; 3 × 12.7 mm Breda-SAFAT machine guns
Bombs weight (kg)
2
 
2,000
39,000
Stat
Number built (qt)
0
 
1
43,000
Introduction 1943
First flight 01.10.1943

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