Search filter

    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      16 m2
      26 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
      4957 kg
      7437 kg
    • Max. takeoff weight (Gross weight)
      10240 kg
      15360 kg
    • Loaded weight
      17064 kg
      25596 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      2 qt
      4 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      1360 km/h
      2040 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
      3058 l
      4588 l
    • Fuel External
      656 l
      986 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      50 kN/kg
      77 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      33 kN
      51 kN
    • Service ceiling
      12192 m
      18288 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2296 km
      3444 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      333 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
      8536 m/min
      12804 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
      1 qt
      250 qt
    • Missiles
      1 qt
      3 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
      72 qt
      108 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi T-2

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
17.9
88.7
Height (m)
0.6
 
4.4
50.1
Wings
Wing area (m2)
1.1
 
21.2
925
Wingspan (Beam) (m)
0.1
 
7.9
95
Weights
Empty weight (kg)
8
 
6,197
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
12,800
575,000
Loaded weight (kg)
5
 
21,330
242,500
Capacity
Crew (per.)
1
 
2
112
Hardpoints (qt)
1
 
3
2,576
One centreline and two underwing pylons
Speeds
Max. Speed (km/h)
25
 
1,700
28,165
at 10975 m
Fuel
Fuel Capacity (l)
23
 
3,823
320,000
Fuel External (l)
142.5
 
821
10,025
Power
Afterburning thrust (kN/kg)
29.4
 
63.5
980
2 powerplants 31,76 kN each
Thrust (kN)
1.5
 
41.9
1,914
2 powerplants 20,95 kN each
Performance
Service ceiling (m)
0.6
 
15,240
161,544
Range (Ferry range) (km)
4
 
2,870
40,700
Сombat radius (km)
277
 
277
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
10,670
36,000
Combat
Guns (qt)
1
 
1
18
20 mm JM61A1 cannon
Missiles (qt)
1
 
2
24
v
Stat
Number built (qt)
0
 
90
43,000
Introduction 1971
First flight 20.07.1971
Stop production 01.03.2006

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