Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      20 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
      1034 kg
      1552 kg
    • Max. takeoff weight (Gross weight)
      1996 kg
      2994 kg
    • Loaded weight
      1669 kg
      2504 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      3 per.
      5 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      283 km/h
      425 km/h
    • Сruise Speed
      263 km/h
      396 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
      384 hp
      576 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4816 m
      7224 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1287 km
      1931 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
      414 m/min
      622 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
      5056 qt
      7586 qt
    • Price
      118200 USD
      177300 USD

Cessna 310

TypeAircraft
Company

Cessna Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.2
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
16.6
925
Wingspan (Beam) (m)
0.1
 
10.7
95
Weights
Empty weight (kg)
8
 
1,292.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,495
575,000
Loaded weight (kg)
5
 
2,086.5
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
4
400
Speeds
Max. Speed (km/h)
25
 
354.1
28,165
Сruise Speed (km/h)
52
 
329.9
3,087
Power
Total Power (hp)
0.4
 
480
60,000
2 powerplants 240 hp each
Performance
Service ceiling (m)
0.6
 
6,020
161,544
Range (Ferry range) (km)
4
 
1,609
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
518.2
36,000
Stat
Number built (qt)
0
 
6,321
43,000
Price (USD)
41.5
 
147,750
750.0 million
Introduction 1953
First flight 03.01.1953

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