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    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      18 m2
      28 m2
    • Wingspan (Beam)
      10 m
      16 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
      2612 kg
      3920 kg
    • Max. takeoff weight (Gross weight)
      5080 kg
      7621 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.
      400 per.
    • Hardpoints
      2060 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      444 km/h
      668 km/h
    • Сruise Speed
      326 km/h
      490 km/h
    • Stall Speed
      121 km/h
      183 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
      1964 hp
      2946 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4876 m
      7316 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1188 km
      1782 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      592 km
      888 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
      1252 m/min
      1880 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
      3 qt
      5 qt
    • Price
      41 USD
      750000000 USD

Piper PA-48 Enforcer

TypeAircraft
Company

Piper Aircraft

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
10.4
88.7
Height (m)
0.6
 
2.7
50.1
Wings
Wing area (m2)
1.1
 
22.8
925
Wingspan (Beam) (m)
0.1
 
12.6
95
Weights
Empty weight (kg)
8
 
3,265.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,350.3
575,000
Capacity
Crew (per.)
1
 
1
112
Hardpoints (qt)
1
 
2,576
2,576
Speeds
Max. Speed (km/h)
25
 
556
28,165
at 4575
Сruise Speed (km/h)
52
 
408
3,087
Stall Speed (km/h)
40
 
152
257.7
40
 
152
257.7
Power
Total Power (hp)
0.4
 
2,455
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,096
161,544
Range (Ferry range) (km)
4
 
1,485
40,700
Сombat radius (km)
277
 
740
7,210
with two 30 mm gun pods
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,566
36,000
Stat
Number built (qt)
0
 
4
43,000
Introduction 1971
First flight 29.04.1971
Stop production 1984

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