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    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      8 m
      13 m
    • Wing loading
      38 kg/m2
      58 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
      344 kg
      518 kg
    • Max. takeoff weight (Gross weight)
      635 kg
      953 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      112 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      3 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      52 km/h
      3087 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
      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
      80 hp
      120 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3072 m
      4609 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      771 km
      1158 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      176 m
      264 m
    • Landing roll
      114 m
      172 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      146 m/min
      220 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
      3 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
      3008 qt
      4512 qt
    • Price
      2396 USD
      3594 USD

Piper PA-12 Super Cruiser

TypeAircraft
Company

Piper Aircraft

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
7.0
88.7
Height (m)
0.6
 
2.1
50.1
Wings
Wingspan (Beam) (m)
0.1
 
10.8
95
Wing loading (kg/m2)
3.1
 
47.9
829
Weights
Empty weight (kg)
8
 
430.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
793.8
575,000
Capacity
Capacity passengers (per.)
1
 
2
400
Speeds
Stall Speed (km/h)
40
 
79
257.7
Power
Total Power (hp)
0.4
 
100
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
3,840.5
161,544
Range (Ferry range) (km)
4
 
964.9
40,700
Takeoff roll (m)
20
 
220
3,200
Landing roll (m)
20
 
143
2,570
Dynamic Performance
Rate of climb (m/min)
1.9
 
182.9
36,000
Propellers
Propellers (qt)
1
 
1
8
Prop diameter (m)
1.8
 
1.9
5.8
Stat
Number built (qt)
0
 
3,760
43,000
Price (USD)
41.5
 
2,995
750.0 million
Introduction 1946
First flight 29.10.1945

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