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    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      60 m2
      91 m2
    • Wingspan (Beam)
      14 m
      22 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
      1451 kg
      2177 kg
    • Max. takeoff weight (Gross weight)
      2200 kg
      3302 kg
    • Loaded weight
      2200 kg
      3302 kg
    • Crew
      2 per.
      4 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
      124 km/h
      188 km/h
    • Сruise Speed
      105 km/h
      159 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
      259 hp
      389 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      0 m
      161544 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
      5 h
      9 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
      128 m/min
      193 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
      3 qt
      5 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Avro Pike

TypeAircraft
Company

Avro Aircraft

Scheme

Biplane

Geometry
Length (m)
1.9
 
11.9
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
75.7
925
Wingspan (Beam) (m)
0.1
 
18.3
95
Weights
Empty weight (kg)
8
 
1,814
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,751
575,000
Loaded weight (kg)
5
 
2,751
242,500
Capacity
Crew (per.)
1
 
3
112
pilot and two gunners
Speeds
Max. Speed (km/h)
25
 
156
28,165
Сruise Speed (km/h)
52
 
132
3,087
Power
Total Power (hp)
0.4
 
324
60,000
2 powerplants 162 hp each
Performance
Endurance (h)
0.0
 
7
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
160.3
36,000
Combat
Guns (qt)
1
 
4
18
1 × flexible .303 in (7.7 mm) Lewis Gun in nose; 1 × flexible .303 in (7.7 mm) Lewis gun in rear fuselage; 2 × 112 lb (51 kg) bombs carried in internal bay
Stat
Number built (qt)
0
 
2
43,000
Introduction 1916
First flight 01.05.1916

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