Search filter

    • Year
      1906
      2018
    • Length
      4 m
      8 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      12 m2
      20 m2
    • Wingspan (Beam)
      6 m
      10 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
      758 kg
      1138 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1007 kg
      1512 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
      227 km/h
      341 km/h
    • Сruise Speed
      179 km/h
      269 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
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      350 hp
      526 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4640 m
      6960 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      382 km
      574 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
      412 m/min
      620 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
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      5 qt
      9 qt
    • Price
      41 USD
      750000000 USD

Curtiss F9C Sparrowhawk

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
6.2
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
16.1
925
Wingspan (Beam) (m)
0.1
 
7.8
95
Wing loading (kg/m2)
3.1
 
78
829
Weights
Empty weight (kg)
8
 
947.6
276,800
Loaded weight (kg)
5
 
1,259.2
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
284.1
28,165
Сruise Speed (km/h)
52
 
224
3,087
Power
Power/mass (hp/kg)
0.0
 
0.4
22.1
Total Power (hp)
0.4
 
438
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,800
161,544
Range (Ferry range) (km)
4
 
478
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
516
36,000
Combat
Guns (qt)
1
 
2
18
.30 in (7.62 mm) Browning machine guns
Stat
Number built (qt)
0
 
7
43,000
Introduction 1931
First flight 12.02.1931
Stop production 1937

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