Search filter

    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      20 m2
      32 m2
    • Wingspan (Beam)
      9 m
      15 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
      2293 kg
      3441 kg
    • Max. takeoff weight (Gross weight)
      3265 kg
      4899 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.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      403 km/h
      605 km/h
    • Сruise Speed
      168 km/h
      252 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
      1080 hp
      1620 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9095 m
      13643 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      804 km
      1208 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
      609 m/min
      915 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
      3 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
      461 qt
      693 qt
    • Price
      41 USD
      750000000 USD

Curtiss SC Seahawk

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
11.1
88.7
Height (m)
0.6
 
4.9
50.1
Wings
Wing area (m2)
1.1
 
26.0
925
Wingspan (Beam) (m)
0.1
 
12.5
95
Weights
Empty weight (kg)
8
 
2,866.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,082
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
504
28,165
at 8700 m
Сruise Speed (km/h)
52
 
210
3,087
Power
Total Power (hp)
0.4
 
1,350
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
11,369.0
161,544
Range (Ferry range) (km)
4
 
1,006
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
762
36,000
Combat
Guns (qt)
1
 
2
18
.50 M2 Browning machine guns
Bombs (qt)
1
 
2
250
150 kg bombs
Stat
Number built (qt)
0
 
577
43,000
Introduction 1944
First flight 16.02.1944
Stop production 1949

Similar aircraft

Get more

Comments