Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 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
      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
      1657 kg
      2486 kg
    • Max. takeoff weight (Gross weight)
      2180 kg
      3272 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 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
      400 km/h
      600 km/h
    • Сruise Speed
      368 km/h
      552 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
      840 hp
      1260 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7973 m
      11961 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      804 km
      1208 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
      829 m/min
      1244 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
      3 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
      172 qt
      258 qt
    • Price
      18400 USD
      27600 USD

Curtiss P-36 Hawk

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.7
88.7
Height (m)
0.6
 
2.6
50.1
Wings
Wing area (m2)
1.1
 
21.9
925
Wingspan (Beam) (m)
0.1
 
11.4
95
Weights
Empty weight (kg)
8
 
2,071.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,726.1
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
500
28,165
at 2960 m
Сruise Speed (km/h)
52
 
460
3,087
Power
Total Power (hp)
0.4
 
1,050
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
9,967.0
161,544
Range (Ferry range) (km)
4
 
1,006
40,700
at 419 km/h
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,036.3
36,000
Combat
Guns (qt)
1
 
2
18
1 × 0.30 in (7.62 mm) M1919 Browning machine gun; 1 × 0.50 in (12.7 mm) M2 Browning machine gun
Stat
Number built (qt)
0
 
215
43,000
Price (USD)
41.5
 
23,000
750.0 million
Introduction 1939
First flight 06.05.1935
Stop production 1954

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