Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      21 m2
    • Wingspan (Beam)
      8 m
      14 m
    • Wing loading
      12 kg/m2
      20 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
      529 kg
      795 kg
    • Max. takeoff weight (Gross weight)
      1053 kg
      1581 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      436 kg
      654 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
      150 km/h
      226 km/h
    • Сruise Speed
      136 km/h
      204 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
      188 hp
      282 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3169 m
      4755 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      400 km
      600 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
      153 m/min
      231 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
      4133 qt
      6201 qt
    • Price
      41 USD
      750000000 USD

Piper PA-25 Pawnee

TypeAircraft
Company

Piper Aircraft

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
7.6
88.7
Height (m)
0.6
 
2.2
50.1
Wings
Wing area (m2)
1.1
 
17
925
Wingspan (Beam) (m)
0.1
 
11.0
95
Wing loading (kg/m2)
3.1
 
15.9
829
Weights
Empty weight (kg)
8
 
662
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,317
575,000
Capacity
Crew (per.)
1
 
1
112
Useful load (kg)
26.4
 
545
90,700
Speeds
Max. Speed (km/h)
25
 
188
28,165
Сruise Speed (km/h)
52
 
170
3,087
Power
Total Power (hp)
0.4
 
235
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
3,962
161,544
Range (Ferry range) (km)
4
 
500
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
192
36,000
at MTOW
Stat
Number built (qt)
0
 
5,167
43,000
Introduction 1957
First flight 1957

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