Search filter

    • Year
      1906
      2018
    • Length
      10 m
      15 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      14 m
      22 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
      3414 kg
      5122 kg
    • Max. takeoff weight (Gross weight)
      4779 kg
      7169 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
      318 km/h
      478 km/h
    • Сruise Speed
      279 km/h
      419 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
      1360 hp
      2040 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6696 m
      10044 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      838 km
      1258 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
      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
      6 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      217 kg
      327 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      10 qt
      16 qt
    • Price
      84000 USD
      126000 USD

Curtiss A-18 Shrike

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
12.5
88.7
Height (m)
0.6
 
3.5
50.1
Wings
Wingspan (Beam) (m)
0.1
 
18.1
95
Weights
Empty weight (kg)
8
 
4,268.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,973.8
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
398
28,165
Сruise Speed (km/h)
52
 
349
3,087
Power
Total Power (hp)
0.4
 
1,700
60,000
2 powerplants 850 hp each
Performance
Service ceiling (m)
0.6
 
8,370
161,544
Range (Ferry range) (km)
4
 
1,048
40,700
Combat
Guns (qt)
1
 
5
18
4 × forward-firing .30 in (7.62 mm) M1919 Browning machine guns; 1 × aft-firing .30 in (7.62 mm) machine gun
Bombs weight (kg)
2
 
272
39,000
181 kg bombs in two wing bays; 91 kg bombs or chemical smoke tanks underwing
Stat
Number built (qt)
0
 
13
43,000
Price (USD)
41.5
 
105,000
750.0 million
Introduction 1935
First flight 01.09.1935
Stop production 1943

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