Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      55 m2
      84 m2
    • Wingspan (Beam)
      13 m
      20 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
      8 kg
      276800 kg
    • Max. takeoff weight (Gross weight)
      4120 kg
      6180 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
      196 km/h
      294 km/h
    • Сruise Speed
      52 km/h
      3087 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
      679 hp
      1020 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3200 m
      4800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1920 km
      2880 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      9 h
      14 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
      42 min
      65 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
      4 qt
      8 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
      39 qt
      59 qt
    • Price
      41 USD
      750000000 USD

SIAI Savoia-Marchetti S.78

TypeAircraft
Company

SIAI-Marchetti

Scheme

Biplane

Geometry
Length (m)
1.9
 
12.3
88.7
Height (m)
0.6
 
4.3
50.1
Wings
Wing area (m2)
1.1
 
69.5
925
Wingspan (Beam) (m)
0.1
 
16.7
95
Weights
Max. takeoff weight (Gross weight) (kg)
154
 
5,150
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
245
28,165
Power
Total Power (hp)
0.4
 
849.9
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,000
161,544
Range (Ferry range) (km)
4
 
2,400
40,700
Endurance (h)
0.0
 
11.5
150
Dynamic Performance
Time to altitude (min)
0.6
 
5.6
105
to 1000 m
0.6
 
14.5
105
to 2000 m
0.6
 
29.7
105
to 3000 m
0.6
 
53.7
105
to 3800 m
Combat
Guns (qt)
1
 
4
18
7.7 mm (.303 in) machine guns
Bombs (qt)
1
 
6
250
100 kg bomb load
Stat
Number built (qt)
0
 
49
43,000
First flight 1932

Similar aircraft

Get more

Comments