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
      22 m2
      34 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
      669 kg
      1004 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      904 kg
      1358 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 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
      154 km/h
      232 km/h
    • Сruise Speed
      124 km/h
      188 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
      192 hp
      288 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3901 m
      5853 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      321 km
      483 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
      221 m/min
      333 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
      484 qt
      728 qt
    • Price
      41 USD
      750000000 USD

Avro Tutor

TypeAircraft
Company

Avro Aircraft

Scheme

Biplane

Geometry
Length (m)
1.9
 
8.0
88.7
Height (m)
0.6
 
2.9
50.1
Wings
Wing area (m2)
1.1
 
28.0
925
Wingspan (Beam) (m)
0.1
 
10.4
95
Weights
Empty weight (kg)
8
 
836.4
276,800
Loaded weight (kg)
5
 
1,131
242,500
Capacity
Crew (per.)
1
 
2
112
student & instructor
Speeds
Max. Speed (km/h)
25
 
193
28,165
Сruise Speed (km/h)
52
 
156
3,087
Power
Total Power (hp)
0.4
 
240
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,876.8
161,544
Range (Ferry range) (km)
4
 
402
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
277.4
36,000
Stat
Number built (qt)
0
 
606
43,000
Introduction 1929
First flight 1929
Stop production 1941

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