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    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      9 m2
      14 m2
    • Wingspan (Beam)
      8 m
      13 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
      409 kg
      614 kg
    • Max. takeoff weight (Gross weight)
      606 kg
      909 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.
      2 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      161 km/h
      243 km/h
    • Сruise Speed
      148 km/h
      222 km/h
    • Stall Speed
      72 km/h
      110 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      204 km/h
      308 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
      89 hp
      135 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3200 m
      4800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      693 km
      1041 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
      175 m/min
      263 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
      18 qt
    • Bombs
      1 qt
      250 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
      1987 qt
      2981 qt
    • Price
      41 USD
      750000000 USD

Piper PA-38 Tomahawk

TypeAircraft
Company

Piper Aircraft

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
7.0
88.7
Height (m)
0.6
 
2.8
50.1
Wings
Wing area (m2)
1.1
 
11.6
925
Wingspan (Beam) (m)
0.1
 
10.4
95
Weights
Empty weight (kg)
8
 
511.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
757.5
575,000
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
1
400
Speeds
Max. Speed (km/h)
25
 
202
28,165
Сruise Speed (km/h)
52
 
185
3,087
at 3200 m at 65% power
Stall Speed (km/h)
40
 
91
257.7
flaps down
Never exceed speed (km/h)
108.0
 
256
1,050
Power
Total Power (hp)
0.4
 
112
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,000
161,544
Range (Ferry range) (km)
4
 
867
40,700
at 3200 m at 65% power
Dynamic Performance
Rate of climb (m/min)
1.9
 
219
36,000
Stat
Number built (qt)
0
 
2,484
43,000
Introduction 1977

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