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
      15 m2
      24 m2
    • Wingspan (Beam)
      9 m
      15 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
      1528 kg
      2294 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1946 kg
      2920 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
      283 km/h
      425 km/h
    • Сruise Speed
      247 km/h
      371 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
      480 hp
      720 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5120 m
      7681 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      901 km
      1353 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
      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
      162 qt
      244 qt
    • Price
      24800 USD
      37200 USD

Curtiss O-52 Owl

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
8.0
88.7
Height (m)
0.6
 
2.8
50.1
Wings
Wing area (m2)
1.1
 
19.6
925
Wingspan (Beam) (m)
0.1
 
12.4
95
Weights
Empty weight (kg)
8
 
1,911.0
276,800
Loaded weight (kg)
5
 
2,433
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
354
28,165
Сruise Speed (km/h)
52
 
309
3,087
Power
Total Power (hp)
0.4
 
600
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,400.8
161,544
Range (Ferry range) (km)
4
 
1,127
40,700
Combat
Guns (qt)
1
 
2
18
1 × forward and 1 × rearward firing .30-cal (7.62 mm) machine gun
Stat
Number built (qt)
0
 
203
43,000
Price (USD)
41.5
 
31,000
750.0 million
Introduction 1941
First flight 1940

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