Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      20 m2
    • Wingspan (Beam)
      8 m
      14 m
    • Wing loading
      89 kg/m2
      135 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
      835 kg
      1254 kg
    • Max. takeoff weight (Gross weight)
      1451 kg
      2178 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      4 per.
      6 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      302 km/h
      454 km/h
    • Сruise Speed
      286 km/h
      430 km/h
    • Stall Speed
      86 km/h
      130 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
      248 hp
      372 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6583 m
      9876 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1334 km
      2002 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
      226 m/min
      341 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
      7392 qt
      11088 qt
    • Price
      41 USD
      750000000 USD

Cessna 210

TypeAircraft
Company

Cessna Aircraft Company

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
8.6
88.7
Height (m)
0.6
 
3.0
50.1
Wings
Wing area (m2)
1.1
 
16.3
925
Wingspan (Beam) (m)
0.1
 
11.2
95
Wing loading (kg/m2)
3.1
 
111.8
829
Weights
Empty weight (kg)
8
 
1,044.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,814.4
575,000
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
5
400
Speeds
Max. Speed (km/h)
25
 
378
28,165
at 5200 m
Сruise Speed (km/h)
52
 
358
3,087
at 6100 m
Stall Speed (km/h)
40
 
108
257.7
flaps down, power off
Power
Total Power (hp)
0.4
 
310
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,229.6
161,544
Range (Ferry range) (km)
4
 
1,668
40,700
econ cruise at 3050 m
Dynamic Performance
Rate of climb (m/min)
1.9
 
283.5
36,000
Stat
Number built (qt)
0
 
9,240
43,000
Introduction 1957
First flight 1957

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