Search filter

    • Year
      1906
      2018
    • Length
      5 m
      8 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      10 m2
      17 m2
    • Wingspan (Beam)
      7 m
      11 m
    • Wing loading
      52 kg/m2
      80 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
      402 kg
      605 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      725 kg
      1089 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      2 per.
      4 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      181 km/h
      273 km/h
    • Сruise Speed
      172 km/h
      259 km/h
    • Stall Speed
      63 km/h
      95 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
      109 l
      164 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
      128 hp
      192 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4023 m
      6035 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      644 km
      966 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      2 h
      5 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
      195 m/min
      293 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      3 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
      896 qt
      1344 qt
    • Price
      41 USD
      750000000 USD

Piper PA-20 Pacer

TypeAircraft
Company

Piper Aircraft

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
6.3
88.7
Height (m)
0.6
 
2.5
50.1
Wings
Wing area (m2)
1.1
 
13.7
925
Wingspan (Beam) (m)
0.1
 
8.9
95
Wing loading (kg/m2)
3.1
 
66
829
Weights
Empty weight (kg)
8
 
503.5
276,800
Loaded weight (kg)
5
 
907.2
242,500
5
 
907
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
3
400
Speeds
Max. Speed (km/h)
25
 
226.9
28,165
Сruise Speed (km/h)
52
 
215.7
3,087
75% power
Stall Speed (km/h)
40
 
78.9
257.7
Fuel
Fuel Capacity (l)
23
 
136.3
320,000
Power
Total Power (hp)
0.4
 
160
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,029
161,544
Range (Ferry range) (km)
4
 
805
40,700
with reserves
Endurance (h)
0.0
 
3.5
150
at 65% power with one hour reserve
Dynamic Performance
Rate of climb (m/min)
1.9
 
243.8
36,000
Propellers
Propellers (qt)
1
 
1
8
Prop blade number (qt)
1
 
2
8
Stat
Number built (qt)
0
 
1,120
43,000
Introduction 1951
First flight 1949

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