Search filter

    • Year
      1906
      2018
    • Length
      9 m
      14 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      12 m
      19 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
      3960 kg
      5940 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      5840 kg
      8760 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
      464 km/h
      696 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
      2400 hp
      3600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8000 m
      12000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1600 km
      2400 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
      571 m/min
      857 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
      3 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
      190 qt
      286 qt
    • Price
      41 USD
      750000000 USD

Kawasaki Ki-102

TypeAircraft
Company

Kawasaki Heavy Industries

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
11.5
88.7
Height (m)
0.6
 
3.7
50.1
Wings
Wingspan (Beam) (m)
0.1
 
15.6
95
Weights
Empty weight (kg)
8
 
4,950
276,800
Loaded weight (kg)
5
 
7,300
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
580
28,165
Power
Total Power (hp)
0.4
 
3,000
60,000
2 powerplants 1500 hp each
Performance
Service ceiling (m)
0.6
 
10,000
161,544
Range (Ferry range) (km)
4
 
2,000
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
714
36,000
Combat
Guns (qt)
1
 
4
18
1 × 57 mm (2.24 in) Ho-401 cannon—replaced in the 102a with a 37 mm (1.46 in) cannon, deleted in the 102c; 2 × 20 mm Ho-5 cannon in the belly—replaced in the 102c with 30 mm (1.18 in) cannons in the package, plus oblique-firing 2 × 20 mm cannons; 1 × 12.7 mm (0.50 in) Ho-103 machine gun—deleted in the 102a and 102c
Bombs (qt)
1
 
2
250
250 kg (551 lb) bombs or 2 x 200 L (53 US gal) drop tanks
Stat
Number built (qt)
0
 
238
43,000
Introduction 1944
First flight 1944
Stop production 1945

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