Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      21 m2
      32 m2
    • Wingspan (Beam)
      10 m
      17 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
      1414 kg
      2122 kg
    • Max. takeoff weight (Gross weight)
      2088 kg
      3134 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
      228 km/h
      342 km/h
    • Сruise Speed
      196 km/h
      296 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
      552 hp
      829 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3694 m
      5542 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      670 km
      1006 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
      284 m/min
      428 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
      3 qt
      5 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
      36 qt
      56 qt
    • Price
      41 USD
      750000000 USD

Curtiss A-12 Shrike

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
9.8
88.7
Height (m)
0.6
 
2.8
50.1
Wings
Wing area (m2)
1.1
 
26.4
925
Wingspan (Beam) (m)
0.1
 
13.4
95
Weights
Empty weight (kg)
8
 
1,768.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,610.9
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
285
28,165
Сruise Speed (km/h)
52
 
246
3,087
Power
Total Power (hp)
0.4
 
690.4
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,617.7
161,544
Range (Ferry range) (km)
4
 
838
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
356
36,000
Combat
Guns (qt)
1
 
5
18
4 × forward-firing .30 in (7.62 mm) machine guns; 1 × aft-firing .30 in (7.62 mm) machine gun
Bombs (qt)
1
 
4
250
55 kg bombs on underwing racks
Stat
Number built (qt)
0
 
46
43,000
Introduction 1931
Stop production 1942

Similar aircraft

Get more

Comments