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    • 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
      19 m2
      30 m2
    • Wingspan (Beam)
      7 m
      12 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
      1206 kg
      1811 kg
    • Max. takeoff weight (Gross weight)
      1651 kg
      2478 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
      289 km/h
      435 km/h
    • Сruise Speed
      202 km/h
      304 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
      616 hp
      924 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6583 m
      9876 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      933 km
      1401 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      360 km
      542 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
      524 m/min
      787 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
      131 qt
      197 qt
    • Price
      41 USD
      750000000 USD

Curtiss BF2C Goshawk

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
7.2
88.7
Height (m)
0.6
 
3.0
50.1
Wings
Wing area (m2)
1.1
 
24.3
925
Wingspan (Beam) (m)
0.1
 
9.6
95
Weights
Empty weight (kg)
8
 
1,508.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,064.8
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
362
28,165
Сruise Speed (km/h)
52
 
253
3,087
Power
Total Power (hp)
0.4
 
770
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,229.6
161,544
Range (Ferry range) (km)
4
 
1,167
40,700
Сombat radius (km)
277
 
451
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
655.3
36,000
Combat
Guns (qt)
1
 
2
18
1x7.62mm M1919 Browning machine gun (Right)+1x12.7mm M2 Browning machine gun
Bombs (qt)
1
 
1
250
215kg bomb on an under-fuselage hardpoin or
1
 
2
250
53kg bombs carried, one under each lower wing
Stat
Number built (qt)
0
 
164
43,000
Introduction 1933
Stop production 1949

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