Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      20 m2
      31 m2
    • Wingspan (Beam)
      11 m
      17 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
      2360 kg
      3540 kg
    • Max. takeoff weight (Gross weight)
      3352 kg
      5028 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 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
      294 km/h
      442 km/h
    • Сruise Speed
      229 km/h
      345 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
      736 hp
      1104 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5200 m
      7800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      696 km
      1044 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
      1 qt
      2 qt
    • Bombs
      1 qt
      2 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
      27 qt
      41 qt
    • Price
      41 USD
      750000000 USD

SIAI Savoia-Marchetti SM.85

TypeAircraft
Company

SIAI-Marchetti

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
10.4
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wing area (m2)
1.1
 
25.8
925
Wingspan (Beam) (m)
0.1
 
14
95
Weights
Empty weight (kg)
8
 
2,950
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,190
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
368
28,165
Сruise Speed (km/h)
52
 
287
3,087
Power
Total Power (hp)
0.4
 
920
60,000
2 powerplants 460 hp each
Performance
Service ceiling (m)
0.6
 
6,500
161,544
Range (Ferry range) (km)
4
 
870
40,700
Combat
Guns (qt)
1
 
1
18
fixed forward 12.7 mm (.5 in) or 7.7 mm (.303 in) machine gun
Bombs (qt)
1
 
1
250
800 kg (1,764 lb) bomb
Stat
Number built (qt)
0
 
34
43,000
Introduction 1936
First flight 19.12.1936
Stop production 1940

Similar aircraft

Get more

Comments