Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      14 m2
      23 m2
    • Wingspan (Beam)
      9 m
      15 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
      1386 kg
      2080 kg
    • Max. takeoff weight (Gross weight)
      2358 kg
      3539 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
      4 per.
      8 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      344 km/h
      518 km/h
    • Сruise Speed
      288 km/h
      432 km/h
    • Stall Speed
      108 km/h
      162 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
      544 hp
      816 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6339 m
      9510 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1672 km
      2508 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
      390 m/min
      586 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
      241 qt
      363 qt
    • Price
      41 USD
      750000000 USD

Cessna 411

TypeAircraft
Company

Cessna Aircraft Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
10.2
88.7
Height (m)
0.6
 
3.5
50.1
Wings
Wing area (m2)
1.1
 
18.6
925
Wingspan (Beam) (m)
0.1
 
12.2
95
Weights
Empty weight (kg)
8
 
1,732.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,948.4
575,000
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
6
400
Speeds
Max. Speed (km/h)
25
 
431
28,165
at 4875
Сruise Speed (km/h)
52
 
360
3,087
at 3050 (75% power)
Stall Speed (km/h)
40
 
135
257.7
flaps down
Power
Total Power (hp)
0.4
 
680
60,000
2 powerplants 340 hp each
Performance
Service ceiling (m)
0.6
 
7,924.8
161,544
Range (Ferry range) (km)
4
 
2,090
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
487.7
36,000
Stat
Number built (qt)
0
 
302
43,000
Introduction 1962
First flight 1962

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