Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      12 m2
      20 m2
    • Wingspan (Beam)
      8 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
      585 kg
      879 kg
    • Max. takeoff weight (Gross weight)
      881 kg
      1323 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
      148 km/h
      222 km/h
    • Сruise Speed
      133 km/h
      201 km/h
    • Stall Speed
      69 km/h
      105 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
      124 l
      187 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
      170 hp
      256 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4511 m
      6767 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      682 km
      1024 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
      280 m/min
      421 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
      18 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
      2744 qt
      4118 qt
    • Price
      41 USD
      750000000 USD

Cessna O-1 Bird Dog

TypeAircraft
Company

Cessna Aircraft Company

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
7.9
88.7
Height (m)
0.6
 
2.2
50.1
Wings
Wing area (m2)
1.1
 
16.2
925
Wingspan (Beam) (m)
0.1
 
11.0
95
Weights
Empty weight (kg)
8
 
732.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,102.2
575,000
Capacity
Crew (per.)
1
 
2
112
1-2
Speeds
Max. Speed (km/h)
25
 
185
28,165
Сruise Speed (km/h)
52
 
167
3,087
Stall Speed (km/h)
40
 
87
257.7
Fuel
Fuel Capacity (l)
23
 
155.2
320,000
Power
Total Power (hp)
0.4
 
213
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,638.8
161,544
Range (Ferry range) (km)
4
 
853
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
350.5
36,000
Stat
Number built (qt)
0
 
3,431
43,000
Introduction 1950
First flight 14.12.1949
Stop production 1974

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