Search filter

    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      8 m2
      13 m2
    • Wingspan (Beam)
      6 m
      11 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
      612 kg
      918 kg
    • Max. takeoff weight (Gross weight)
      880 kg
      1320 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.
      3 per.
    • Hardpoints
      1 qt
      3 qt
    • Ground Speed
      269 km/h
      405 km/h
    • Max. Speed
      352 km/h
      530 km/h
    • Сruise Speed
      240 km/h
      360 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
      169 l
      254 l
    • Fuel External
      142 l
      171 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
      209 hp
      314 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4632 m
      6948 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1640 km
      2460 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
      436 m/min
      656 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
      688 qt
      1032 qt
    • Price
      41 USD
      750000000 USD

SIAI Marchetti SF.250

TypeAircraft
Company

SIAI-Marchetti

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
7.1
88.7
Height (m)
0.6
 
2.4
50.1
Wings
Wing area (m2)
1.1
 
10.1
925
Wingspan (Beam) (m)
0.1
 
8.4
95
Weights
Empty weight (kg)
8
 
765
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,200
575,000
utility
154
 
1,100
575,000
aerobatic
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
2
400
Hardpoints (qt)
1
 
2
2,576
under-wing hard points, each can carry 300 kg
Speeds
Ground Speed (km/h)
96.6
 
337
1,500
Max. Speed (km/h)
25
 
441
28,165
Сruise Speed (km/h)
52
 
300
3,087
Fuel
Fuel Capacity (l)
23
 
211.3
320,000
Fuel External (l)
142.5
 
142.5
10,025
Power
Total Power (hp)
0.4
 
261.4
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,790
161,544
Range (Ferry range) (km)
4
 
2,050
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
546
36,000
Stat
Number built (qt)
0
 
860
43,000
Introduction 01.04.1966
First flight 15.07.1964

Similar aircraft

Get more

Comments