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    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      25 m2
      39 m2
    • Wingspan (Beam)
      8 m
      14 m
    • Wing loading
      62 kg/m2
      94 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
      1374 kg
      2062 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1976 kg
      2966 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
      212 km/h
      320 km/h
    • Сruise Speed
      171 km/h
      257 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
      440 hp
      660 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3633 m
      5450 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      868 km
      1304 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
      223 m/min
      335 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
      3 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      236 kg
      354 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      257 qt
      387 qt
    • Price
      41 USD
      750000000 USD

Curtiss SOC Seagull

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
9.6
88.7
Height (m)
0.6
 
4.5
50.1
Wings
Wing area (m2)
1.1
 
31.8
925
Wingspan (Beam) (m)
0.1
 
11.0
95
Wing loading (kg/m2)
3.1
 
77.7
829
Weights
Empty weight (kg)
8
 
1,718.2
276,800
Loaded weight (kg)
5
 
2,471
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and observer
Speeds
Max. Speed (km/h)
25
 
266
28,165
at 1500 m
Сruise Speed (km/h)
52
 
214
3,087
Power
Total Power (hp)
0.4
 
550
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,541.5
161,544
Range (Ferry range) (km)
4
 
1,086
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
278.9
36,000
Combat
Guns (qt)
1
 
2
18
1× fixed, forward firing 0.30 in (7.62 mm) Browning M2 AN and 1× flexible mounted rear-firing 0.30 in (7.62 mm) Browning M2 AN machine gun
Bombs weight (kg)
2
 
295
39,000
Stat
Number built (qt)
0
 
322
43,000
Introduction 1934
First flight 01.04.1934
Stop production 1945

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