Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      15 m2
      24 m2
    • Wingspan (Beam)
      9 m
      14 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      5
      9
    • 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
      1153 kg
      1731 kg
    • Max. takeoff weight (Gross weight)
      1886 kg
      2831 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      580 kg
      871 kg
    • Capacity passengers
      4 per.
      6 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      276 km/h
      416 km/h
    • Сruise Speed
      222 km/h
      334 km/h
    • Stall Speed
      87 km/h
      131 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
      400 hp
      600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4620 m
      6932 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1956 km
      2934 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
      341 m/min
      513 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      3 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
      5580 qt
      8372 qt
    • Price
      41 USD
      750000000 USD

Piper PA-23

TypeAircraft
Company

Piper Aircraft

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
9.5
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
19.3
925
Wingspan (Beam) (m)
0.1
 
11.3
95
Aspect ratio
1.7
 
6.8
25.6
Weights
Empty weight (kg)
8
 
1,442.4
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,358.7
575,000
Capacity
Crew (per.)
1
 
1
112
Payload (kg)
23
 
725.8
122,470
cargo
Capacity passengers (per.)
1
 
5
400
Speeds
Max. Speed (km/h)
25
 
346
28,165
Сruise Speed (km/h)
52
 
278
3,087
at 3110 m, long-range cruise
Stall Speed (km/h)
40
 
109
257.7
flaps down
Power
Total Power (hp)
0.4
 
500
60,000
2 powerplants 250 hp each
Performance
Service ceiling (m)
0.6
 
5,776.0
161,544
absolute ceiling
Range (Ferry range) (km)
4
 
2,445
40,700
at long-range cruise
Dynamic Performance
Rate of climb (m/min)
1.9
 
426.7
36,000
Propellers
Propellers (qt)
1
 
2
8
Prop blade number (qt)
1
 
2
8
Stat
Number built (qt)
0
 
6,976
43,000
Introduction 1954
First flight 02.03.1952

Similar aircraft

Get more

Comments