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
      12 m2
      20 m2
    • Wingspan (Beam)
      8 m
      14 m
    • Wing loading
      54 kg/m2
      83 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      5
      9
    • 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
      613 kg
      921 kg
    • Max. takeoff weight (Gross weight)
      798 kg
      1198 kg
    • Loaded weight
      889 kg
      1334 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      2 per.
      4 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      173 km/h
      261 km/h
    • Сruise Speed
      180 km/h
      272 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
      241 km/h
      363 km/h
    • Fuel Capacity
      169 l
      255 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
      128 hp
      192 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3280 m
      4920 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1031 km
      1547 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
      175 m/min
      264 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      3 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
      34400 qt
      43000 qt
    • Price
      6960 USD
      10440 USD

Cessna 172

TypeAircraft
Company

Cessna Aircraft Company

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
8.3
88.7
Height (m)
0.6
 
2.7
50.1
Wings
Wing area (m2)
1.1
 
16.2
925
Wingspan (Beam) (m)
0.1
 
10.9
95
Wing loading (kg/m2)
3.1
 
68.6
829
Aspect ratio
1.7
 
7.3
25.6
Weights
Empty weight (kg)
8
 
767.0
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
998
575,000
Loaded weight (kg)
5
 
1,111.3
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
3
400
Speeds
Max. Speed (km/h)
25
 
217
28,165
Сruise Speed (km/h)
52
 
226
3,087
Stall Speed (km/h)
40
 
87
257.7
power off, flaps down
Never exceed speed (km/h)
108.0
 
302
1,050
Fuel
Fuel Capacity (l)
23
 
212
320,000
Power
Total Power (hp)
0.4
 
160
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,100
161,544
Range (Ferry range) (km)
4
 
1,289
40,700
with 45 minute reserve, 55% power, at 3658 m
Dynamic Performance
Rate of climb (m/min)
1.9
 
219.8
36,000
Propellers
Propellers (qt)
1
 
1
8
Prop blade number (qt)
1
 
2
8
Stat
Number built (qt)
0
 
43,000
43,000
Price (USD)
41.5
 
8,700
750.0 million
Introduction 1965

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