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
      13 m2
      21 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
      500 kg
      752 kg
    • Max. takeoff weight (Gross weight)
      852 kg
      1280 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 per.
    • Useful load
      347 kg
      521 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
      208 km/h
      314 km/h
    • Сruise Speed
      192 km/h
      290 km/h
    • Stall Speed
      40 km/h
      258 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
      115 hp
      174 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4388 m
      6582 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1010 km
      1516 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
      244 m/min
      366 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
      182 qt
      274 qt
    • Price
      41 USD
      750000000 USD

Cessna 165

TypeAircraft
Company

Cessna Aircraft Company

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
7.5
88.7
Height (m)
0.6
 
2.4
50.1
Wings
Wing area (m2)
1.1
 
16.8
925
Wingspan (Beam) (m)
0.1
 
10.4
95
Weights
Empty weight (kg)
8
 
626
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,066
575,000
Capacity
Crew (per.)
1
 
4
112
Useful load (kg)
26.4
 
434
90,700
Speeds
Max. Speed (km/h)
25
 
261
28,165
Сruise Speed (km/h)
52
 
241
3,087
Power
Total Power (hp)
0.4
 
144.8
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,485
161,544
Range (Ferry range) (km)
4
 
1,263
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
305
36,000
Stat
Number built (qt)
0
 
228
43,000
Introduction 1935
First flight 01.06.1935

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