Search filter

    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      9 m
      14 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
      718 kg
      1078 kg
    • Max. takeoff weight (Gross weight)
      1150 kg
      1727 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
      200 km/h
      300 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      52 km/h
      3087 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
      328 hp
      492 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5583 m
      8376 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      464 km
      696 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
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      2 min
      3 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
      60 qt
      90 qt
    • Price
      41 USD
      750000000 USD

Curtiss F6C Hawk

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
6.9
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wingspan (Beam) (m)
0.1
 
11.4
95
Weights
Empty weight (kg)
8
 
898.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,438.3
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
250
1,500
Power
Total Power (hp)
0.4
 
410
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,979.9
161,544
Range (Ferry range) (km)
4
 
580
40,700
Dynamic Performance
Time to altitude (min)
0.6
 
2.5
105
to 1520 m
Combat
Guns (qt)
1
 
2
18
fixed .30 in (7.62 mm) Browning machine guns in the forward fuselage
Stat
Number built (qt)
0
 
75
43,000

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