Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      26 m2
      40 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
      1043 kg
      1565 kg
    • Max. takeoff weight (Gross weight)
      1624 kg
      2437 kg
    • Loaded weight
      5 kg
      242500 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
      178 km/h
      269 km/h
    • Сruise Speed
      141 km/h
      213 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
      348 hp
      522 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3438 m
      5158 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      808 km
      1212 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
      231 m/min
      347 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
      4 qt
      8 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      72 kg
      110 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      270 qt
      406 qt
    • Price
      41 USD
      750000000 USD

Curtiss A-3 Falcon

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
8.3
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
32.8
925
Wingspan (Beam) (m)
0.1
 
11.6
95
Weights
Empty weight (kg)
8
 
1,304.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,030.3
575,000
Capacity
Crew (per.)
1
 
2
112
pilot, observer/rear gunner
Speeds
Max. Speed (km/h)
25
 
223.7
28,165
Сruise Speed (km/h)
52
 
177
3,087
Power
Total Power (hp)
0.4
 
435
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,297.7
161,544
Range (Ferry range) (km)
4
 
1,010
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
289.0
36,000
Combat
Guns (qt)
1
 
6
18
4 × forward-firing .30 in (7.62 mm) M1919 Browning machine guns and 2 × flexible 0.30 in (7.62 mm) Lewis machine guns on a Scarff ring
Bombs weight (kg)
2
 
91
39,000
bombs mounted on lower wing racks
Stat
Number built (qt)
0
 
338
43,000
Introduction 1928
Stop production 01.10.1937

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