Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      18 m2
      29 m2
    • Wingspan (Beam)
      12 m
      19 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
      1826 kg
      2740 kg
    • Max. takeoff weight (Gross weight)
      3574 kg
      5362 kg
    • Loaded weight
      3396 kg
      5096 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      9 per.
      15 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      339 km/h
      509 km/h
    • Сruise Speed
      296 km/h
      444 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
      1444 l
      2166 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
      800 hp
      1200 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7316 m
      10974 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1708 km
      2562 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
      451 m/min
      677 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 Reims-Cessna F406

TypeAircraft
Company

Cessna Aircraft Company

Reims Aviation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
11.9
88.7
Height (m)
0.6
 
4.0
50.1
Wings
Wing area (m2)
1.1
 
23.5
925
Wingspan (Beam) (m)
0.1
 
15.1
95
Weights
Empty weight (kg)
8
 
2,283
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,468
575,000
Loaded weight (kg)
5
 
4,246
242,500
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
12
400
Speeds
Max. Speed (km/h)
25
 
424
28,165
Сruise Speed (km/h)
52
 
370
3,087
Fuel
Fuel Capacity (l)
23
 
1,805
320,000
Power
Total Power (hp)
0.4
 
1,000
60,000
2 powerplants 500 hp each
Performance
Service ceiling (m)
0.6
 
9,145
161,544
Range (Ferry range) (km)
4
 
2,135
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
564
36,000
Stat
Introduction 1983
First flight 22.09.1983

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