Search filter

    • Year
      1906
      2018
    • Length
      12 m
      20 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      49 m2
      75 m2
    • Wingspan (Beam)
      16 m
      25 m
    • Wing loading
      132 kg/m2
      198 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
      6160 kg
      9240 kg
    • Max. takeoff weight (Gross weight)
      8400 kg
      12600 kg
    • Loaded weight
      8040 kg
      12060 kg
    • Crew
      4 per.
      8 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
      287 km/h
      431 km/h
    • Max. Speed
      368 km/h
      552 km/h
    • Сruise Speed
      288 km/h
      432 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
      2064 hp
      3096 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6000 m
      9000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2080 km
      3120 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
      254 m/min
      382 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
      6 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      3 qt
    • Bombs weight
      960 kg
      1440 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      992 qt
      1488 qt
    • Price
      41 USD
      750000000 USD

SIAI Savoia-Marchetti SM.79 Sparviero

TypeAircraft
Company

SIAI-Marchetti

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
16.2
88.7
Height (m)
0.6
 
4.1
50.1
Wings
Wing area (m2)
1.1
 
61.7
925
Wingspan (Beam) (m)
0.1
 
20.2
95
Wing loading (kg/m2)
3.1
 
165
829
Weights
Empty weight (kg)
8
 
7,700
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
10,500
575,000
Loaded weight (kg)
5
 
10,050
242,500
Capacity
Crew (per.)
1
 
6
112
pilot, co-pilot, flight engineer/gunner, radio operator, bombardier, rear gunner
Speeds
Ground Speed (km/h)
96.6
 
359
1,500
Max. Speed (km/h)
25
 
460
28,165
at 3790 m
Сruise Speed (km/h)
52
 
360
3,087
Power
Total Power (hp)
0.4
 
2,580
60,000
3 powerplants 860 hp each
Performance
Service ceiling (m)
0.6
 
7,500
161,544
Range (Ferry range) (km)
4
 
2,600
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
318
36,000
Combat
Guns (qt)
1
 
5
18
1 × 20 mm (0.79 in) forward MG 151 cannon; 2 × 12.7 mm (0.5 in) dorsal Breda-SAFAT machine gun 1 at the top, 1 in the belly (The belly gun was optional); 2 × 7.7 mm (0.303 in) machine guns in lateral "waist-gun" ports (optional)
Torpedoes (qt)
1
 
2
4
external 450 millimetres (17.72 in) torpedoes or
Bombs weight (kg)
2
 
1,200
39,000
internal bomb load
Stat
Number built (qt)
0
 
1,240
43,000
Introduction 1934
First flight 28.09.1934
Stop production 1952

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