Search filter

    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      10 m
      17 m
    • Wing loading
      118 kg/m2
      178 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
      1476 kg
      2215 kg
    • Max. takeoff weight (Gross weight)
      2485 kg
      3729 kg
    • Loaded weight
      2491 kg
      3737 kg
    • Crew
      1 per.
      112 per.
    • Useful load
      1009 kg
      1515 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      7 per.
      11 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      342 km/h
      514 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      105 km/h
      159 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      342 km/h
      514 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
      520 hp
      780 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6559 m
      9839 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1888 km
      2832 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
      353 m/min
      531 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Cessna 402

TypeAircraft
Company

Cessna Aircraft Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
11.1
88.7
Height (m)
0.6
 
3.5
50.1
Wings
Wingspan (Beam) (m)
0.1
 
13.5
95
Wing loading (kg/m2)
3.1
 
148
829
Weights
Empty weight (kg)
8
 
1,845.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,107.1
575,000
Loaded weight (kg)
5
 
3,114
242,500
Capacity
Useful load (kg)
26.4
 
1,262
90,700
Capacity passengers (per.)
1
 
9
400
Up to 9 passengers depending on configuration
Speeds
Max. Speed (km/h)
25
 
428
28,165
Stall Speed (km/h)
40
 
132
257.7
Never exceed speed (km/h)
108.0
 
428
1,050
Power
Total Power (hp)
0.4
 
650
60,000
2 powerplants 325 hp each
Performance
Service ceiling (m)
0.6
 
8,199.1
161,544
Range (Ferry range) (km)
4
 
2,360
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
442.0
36,000
Stat
Introduction 1967
First flight 26.08.1965

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