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    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      20 m2
    • Wingspan (Beam)
      10 m
      16 m
    • Wing loading
      95 kg/m2
      143 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
      854 kg
      1282 kg
    • Max. takeoff weight (Gross weight)
      1488 kg
      2232 kg
    • Loaded weight
      1487 kg
      2232 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      4 per.
      6 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      346 km/h
      520 km/h
    • Сruise Speed
      290 km/h
      436 km/h
    • Stall Speed
      85 km/h
      129 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
      363 l
      546 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
      248 hp
      372 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6096 m
      9144 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2304 km
      3456 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
      278 m/min
      419 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Piper PA-46 Malibu

TypeAircraft
Company

Piper Aircraft

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
8.7
88.7
Height (m)
0.6
 
3.4
50.1
Wings
Wing area (m2)
1.1
 
16.3
925
Wingspan (Beam) (m)
0.1
 
13.1
95
Wing loading (kg/m2)
3.1
 
119
829
Weights
Empty weight (kg)
8
 
1,067.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,860
575,000
Loaded weight (kg)
5
 
1,859.7
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
5
400
Speeds
Max. Speed (km/h)
25
 
433
28,165
Сruise Speed (km/h)
52
 
363
3,087
at 55% power
Stall Speed (km/h)
40
 
107
257.7
Fuel
Fuel Capacity (l)
23
 
454.3
320,000
Power
Total Power (hp)
0.4
 
310
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
7,620
161,544
Range (Ferry range) (km)
4
 
2,880
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
348.4
36,000
Stat
Introduction 1982
First flight 30.11.1979

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