Search filter

    • Year
      1906
      2018
    • Length
      7 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      21 m2
    • Wingspan (Beam)
      9 m
      14 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
      824 kg
      1236 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1480 kg
      2220 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      4 per.
      6 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      285 km/h
      429 km/h
    • Сruise Speed
      251 km/h
      377 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
      320 hp
      480 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6480 m
      9720 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1520 km
      2280 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
      480 m/min
      720 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
      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
      9 qt
      15 qt
    • Price
      41 USD
      750000000 USD

SIAI Marchetti S.210

TypeAircraft
Company

SIAI-Marchetti

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
8.8
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wing area (m2)
1.1
 
17.2
925
Wingspan (Beam) (m)
0.1
 
11.6
95
Weights
Empty weight (kg)
8
 
1,030
276,800
Loaded weight (kg)
5
 
1,850
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
5
400
Speeds
Max. Speed (km/h)
25
 
357
28,165
Сruise Speed (km/h)
52
 
314
3,087
Power
Total Power (hp)
0.4
 
400
60,000
2 powerplants 200 hp each
Performance
Service ceiling (m)
0.6
 
8,100
161,544
Range (Ferry range) (km)
4
 
1,900
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
600
36,000
Stat
Number built (qt)
0
 
12
43,000
Introduction 1970
First flight 19.02.1970

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