Search filter

    • Year
      1906
      2018
    • Length
      20 m
      30 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      20 m2
    • Wingspan (Beam)
      8 m
      14 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
      643 kg
      966 kg
    • Max. takeoff weight (Gross weight)
      1161 kg
      1742 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      517 kg
      777 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
      244 km/h
      368 km/h
    • Сruise Speed
      238 km/h
      358 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
      208 hp
      312 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4754 m
      7133 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1574 km
      2363 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
      321 m/min
      483 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
      3885 qt
      5829 qt
    • Price
      14280 USD
      21420 USD

Piper PA-24 Comanche

TypeAircraft
Company

Piper Aircraft

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
25
88.7
Height (m)
0.6
 
2.3
50.1
Wings
Wing area (m2)
1.1
 
16.5
925
Wingspan (Beam) (m)
0.1
 
11.0
95
Weights
Empty weight (kg)
8
 
804.2
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,451.5
575,000
Capacity
Crew (per.)
1
 
1
112
Useful load (kg)
26.4
 
647
90,700
Capacity passengers (per.)
1
 
3
400
Speeds
Max. Speed (km/h)
25
 
306
28,165
Сruise Speed (km/h)
52
 
298
3,087
Power
Total Power (hp)
0.4
 
260
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,943.6
161,544
Range (Ferry range) (km)
4
 
1,968.7
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
402
36,000
Stat
Number built (qt)
0
 
4,857
43,000
Price (USD)
41.5
 
17,850
750.0 million
Introduction 1956
First flight 24.05.1956

Similar aircraft

Get more

Comments