Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      28 m2
      43 m2
    • Wingspan (Beam)
      8 m
      14 m
    • Wing loading
      47 kg/m2
      71 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
      1037 kg
      1557 kg
    • Max. takeoff weight (Gross weight)
      1650 kg
      2476 kg
    • Loaded weight
      1646 kg
      2470 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
      222 km/h
      334 km/h
    • Сruise Speed
      186 km/h
      280 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
      5364 m
      8047 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      746 km
      1120 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
      358 m/min
      538 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
      3 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      90 kg
      136 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Avro 604 Antelope

TypeAircraft
Company

Avro Aircraft

Scheme

Biplane

Geometry
Length (m)
1.9
 
9.5
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wing area (m2)
1.1
 
35.0
925
Wingspan (Beam) (m)
0.1
 
11.0
95
Wing loading (kg/m2)
3.1
 
58.9
829
Weights
Empty weight (kg)
8
 
1,296.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,063
575,000
Loaded weight (kg)
5
 
2,058
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
278
28,165
Сruise Speed (km/h)
52
 
233
3,087
Power
Total Power (hp)
0.4
 
480
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,705.6
161,544
Range (Ferry range) (km)
4
 
933
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
448.1
36,000
Combat
Guns (qt)
1
 
2
18
1 × synchronised, forward-firing .303 in (7.7 mm) Vickers machine gun; 1 × flexible .303 in (7.7 mm) Lewis Gun in rear cockpit
Bombs weight (kg)
2
 
113
39,000
Stat
Number built (qt)
0
 
1
43,000
Introduction 1928
First flight 01.07.1928
Stop production 01.09.1933

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