Search filter

    • Year
      1906
      2018
    • Length
      11 m
      17 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      20 m2
      31 m2
    • Wingspan (Beam)
      6 m
      10 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
      4640 kg
      6960 kg
    • Max. takeoff weight (Gross weight)
      10400 kg
      15600 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      5 qt
      9 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      1280 km/h
      1920 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
      60 kN/kg
      90 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      44 kN
      67 kN
    • Service ceiling
      12200 m
      18300 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      2960 km
      4440 km
    • Сombat radius
      1040 km
      1560 km
    • Endurance
      2 h
      4 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      7 G
      9 G
    • Rate of climb
      1 m/min
      36000 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
      2 qt
    • Bombs
      19 qt
      29 qt
    • Missiles
      8 qt
      14 qt
    • Rockets
      3 qt
      5 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Airbus Mako/High Energy Advanced Trainer

TypeAircraft
Company

Airbus Group

Scheme

Midwing

Concept

Monoplane

Geometry
Length (m)
1.9
 
13.8
88.7
Height (m)
0.6
 
4.5
50.1
Wings
Wing area (m2)
1.1
 
25.1
925
Wingspan (Beam) (m)
0.1
 
8.3
95
without wingtip missiles
Weights
Empty weight (kg)
8
 
5,800
276,800
in trainer variant
Max. takeoff weight (Gross weight) (kg)
154
 
13,000
575,000
Capacity
Crew (per.)
1
 
1
112
attack variant
1
 
2
112
trainer
Hardpoints (qt)
1
 
7
2,576
with a capacity of 4500 kg
Speeds
Max. Speed (km/h)
25
 
1,600
28,165
Power
Afterburning thrust (kN/kg)
29.4
 
75
980
1 powerplant
Thrust (kN)
1.5
 
55.6
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
15,250
161,544
Range PTB (Ferry range) (km)
720
 
3,700
10,000
Сombat radius (km)
277
 
1,300
7,210
Endurance (h)
0.0
 
3.1
150
Dynamic Performance
Load factor from (G)
2
 
9
9
Combat
Guns (qt)
1
 
1
18
27 mm gun
Bombs (qt)
1
 
24
250
Up to 12× Mk.82, 8× Mk.83, 4× GBU 16
Missiles (qt)
1
 
11
24
4× AIM-9, IRIS-T or ASRAAM, AMRAAM, FMRAAM or Mica, 5x AGM-65 Maverick, 2× anti-ship missile
Rockets (qt)
1
 
4
76
Stat
Introduction 2000

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