Search filter

    • Year
      1906
      2018
    • Length
      13 m
      21 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
      7040 kg
      10560 kg
    • Max. takeoff weight (Gross weight)
      10107 kg
      15161 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 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
      352 km/h
      528 km/h
    • Сruise Speed
      302 km/h
      454 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
      2401 hp
      3603 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5360 m
      8040 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      576 km
      864 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
      259 m/min
      389 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
      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
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

SIAI Savoia-Marchetti SM.89

TypeAircraft
Company

SIAI-Marchetti

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
16.9
88.7
Height (m)
0.6
 
4.5
50.1
Wings
Wing area (m2)
1.1
 
61
925
Wingspan (Beam) (m)
0.1
 
21.0
95
Weights
Empty weight (kg)
8
 
8,800
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
12,634
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
440
28,165
Сruise Speed (km/h)
52
 
378
3,087
Power
Total Power (hp)
0.4
 
3,002
60,000
2 powerplants 1501 hp each
Performance
Service ceiling (m)
0.6
 
6,700
161,544
Range (Ferry range) (km)
4
 
720
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
324
36,000
Combat
Guns (qt)
1
 
6
18
two 54 mm (2.126 in) cannon; two fixed forward firing 12.7 mm (0.500 in) machine guns; two 12.7 mm (0.500 in) machine-guns in dorsal and ventral positions.
Stat
Number built (qt)
0
 
1
43,000
Introduction 1942
First flight 1941

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