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    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      8 m
      13 m
    • Wing loading
      40 kg/m2
      62 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
      392 kg
      589 kg
    • Max. takeoff weight (Gross weight)
      606 kg
      909 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      112 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      2 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      163 km/h
      245 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      63 km/h
      95 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
      88 hp
      132 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3584 m
      5377 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      614 km
      922 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      176 m
      266 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      174 m/min
      262 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
      6067 qt
      9101 qt
    • Price
      41 USD
      750000000 USD

Cessna 152

TypeAircraft
Company

Cessna Aircraft Company

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
7.3
88.7
Height (m)
0.6
 
2.6
50.1
Wings
Wingspan (Beam) (m)
0.1
 
10.2
95
Wing loading (kg/m2)
3.1
 
51
829
Weights
Empty weight (kg)
8
 
490.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
757.5
575,000
Capacity
Capacity passengers (per.)
1
 
1
400
Speeds
Max. Speed (km/h)
25
 
204
28,165
Stall Speed (km/h)
40
 
79
257.7
unpowered, flaps down
Power
Total Power (hp)
0.4
 
110
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,480.6
161,544
Range (Ferry range) (km)
4
 
768
40,700
Takeoff roll (m)
20
 
221
3,200
Dynamic Performance
Rate of climb (m/min)
1.9
 
217.9
36,000
Stat
Number built (qt)
0
 
7,584
43,000

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