Search filter

    • Year
      1906
      2018
    • Length
      11 m
      17 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      18 m2
      28 m2
    • Wingspan (Beam)
      7 m
      12 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
      4535 kg
      6804 kg
    • Max. takeoff weight (Gross weight)
      11248 kg
      16874 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      6 qt
      10 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      874 km/h
      1312 km/h
    • Сruise Speed
      52 km/h
      3087 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
      0 hp
      60000 hp
    • Thrust
      77 kN
      117 kN
    • Service ceiling
      12136 m
      18204 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2604 km
      3908 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
      3588 m/min
      5383 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
      4 qt
      8 qt
    • Rockets
      60 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      114 qt
      172 qt
    • Price
      41 USD
      750000000 USD

Boeing Harrier II

TypeAircraft
Company

Boeing

British Aerospace

McDonnell Douglas

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
14.1
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
22.6
925
Wingspan (Beam) (m)
0.1
 
9.3
95
Weights
Empty weight (kg)
8
 
5,669.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,595.6
575,000
VTO
154
 
14,061
575,000
STO
Capacity
Crew (per.)
1
 
1
112
Hardpoints (qt)
1
 
8
2,576
Speeds
Max. Speed (km/h)
25
 
1,093
28,165
Power
Thrust (kN)
1.5
 
96.7
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
15,170
161,544
Range (Ferry range) (km)
4
 
3,256
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
4,485.1
36,000
Combat
Guns (qt)
1
 
2
18
25 mm ADEN cannon pods under the fuselage
Missiles (qt)
1
 
6
24
AIM-9 Sidewinders or 4× AGM-65 Maverick
Rockets (qt)
1
 
76
76
CRV7 70 mm rockets
Stat
Number built (qt)
0
 
143
43,000
Introduction 1979
First flight 30.04.1985
Stop production 01.03.2011

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