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    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      160 m2
      242 m2
    • Wingspan (Beam)
      23 m
      36 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
      4630 kg
      6946 kg
    • Max. takeoff weight (Gross weight)
      7228 kg
      10843 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      6 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
      148 km/h
      222 km/h
    • Сruise Speed
      124 km/h
      186 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
      1040 hp
      1560 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2377 m
      3567 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      60 m/min
      90 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
      2 qt
      4 qt
    • Bombs
      3 qt
      5 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      2 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Avro Ava

TypeAircraft
Company

Avro Aircraft

Scheme

Biplane

Geometry
Length (m)
1.9
 
17.8
88.7
Height (m)
0.6
 
6.0
50.1
Wings
Wing area (m2)
1.1
 
201
925
Wingspan (Beam) (m)
0.1
 
29.5
95
Weights
Empty weight (kg)
8
 
5,787.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
9,035.6
575,000
Capacity
Crew (per.)
1
 
5
112
Speeds
Max. Speed (km/h)
25
 
185
28,165
Сruise Speed (km/h)
52
 
155
3,087
Power
Total Power (hp)
0.4
 
1,300
60,000
2 powerplants 650 hp each
Performance
Service ceiling (m)
0.6
 
2,972
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
75
36,000
Combat
Guns (qt)
1
 
3
18
0.303 in (7.7 mm) Lewis Guns (Nose, dorsal and retractable ventral positions)
Bombs (qt)
1
 
4
250
250 kg bombs or
Torpedoes (qt)
1
 
1
4
553 mm torpedo
Stat
Number built (qt)
0
 
2
43,000
Introduction 1924
First flight 1924

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