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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
      12 m2
      18 m2
    • Wingspan (Beam)
      8 m
      13 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
      407 kg
      611 kg
    • Max. takeoff weight (Gross weight)
      580 kg
      871 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
      161 km/h
      243 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      123 km/h
      185 km/h
    • Stall Speed
      62 km/h
      94 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      207 km/h
      311 km/h
    • Fuel Capacity
      115 l
      174 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
      80 hp
      120 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3440 m
      5160 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      622 km
      934 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
      163 m/min
      246 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
      19159 qt
      28739 qt
    • Price
      20000 USD
      30000 USD

Cessna 150

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
Wing area (m2)
1.1
 
15
925
Wingspan (Beam) (m)
0.1
 
10.2
95
Weights
Empty weight (kg)
8
 
508.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
725.8
575,000
Capacity
Crew (per.)
1
 
2
112
+ two children not exceeding 120 lb (54 kg)
Speeds
Ground Speed (km/h)
96.6
 
202
1,500
Сruise Speed (km/h)
52
 
154
3,087
at 3050 m
Stall Speed (km/h)
40
 
78
257.7
flaps down, power off
Never exceed speed (km/h)
108.0
 
259
1,050
Fuel
Fuel Capacity (l)
23
 
144.2
320,000
Power
Total Power (hp)
0.4
 
100
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,300
161,544
Range (Ferry range) (km)
4
 
778
40,700
econ cruise, standard fuel
Dynamic Performance
Rate of climb (m/min)
1.9
 
204.2
36,000
Stat
Number built (qt)
0
 
23,949
43,000
Price (USD)
41.5
 
25,000
750.0 million
Introduction 1966
First flight 12.09.1957

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