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
      13 m2
      21 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
      2253 kg
      3381 kg
    • Max. takeoff weight (Gross weight)
      5080 kg
      7621 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
      6 qt
      10 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      652 km/h
      980 km/h
    • Сruise Speed
      629 km/h
      945 km/h
    • Stall Speed
      145 km/h
      219 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
      0 hp
      60000 hp
    • Thrust
      20 kN
      31 kN
    • Service ceiling
      10183 m
      15276 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1184 km
      1776 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      592 km
      888 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
      1704 m/min
      2556 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
      2 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      22 qt
      34 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      192 kg
      290 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      461 qt
      693 qt
    • Price
      41 USD
      750000000 USD

Cessna A-37 Dragonfly

TypeAircraft
Company

Cessna Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.6
88.7
Height (m)
0.6
 
2.7
50.1
Wings
Wing area (m2)
1.1
 
17.1
925
Wingspan (Beam) (m)
0.1
 
10.9
95
Weights
Empty weight (kg)
8
 
2,817.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,350.3
575,000
Capacity
Crew (per.)
1
 
1
112
Hardpoints (qt)
1
 
8
2,576
under-wing with a capacity of 1,230 kg
Speeds
Max. Speed (km/h)
25
 
816
28,165
at 4 877 m
Сruise Speed (km/h)
52
 
787
3,087
at 7 620 m
Stall Speed (km/h)
40
 
182
257.7
Power
Thrust (kN)
1.5
 
25.4
1,914
2 powerplant 12,7 kN each
Performance
Service ceiling (m)
0.6
 
12,730.0
161,544
Range (Ferry range) (km)
4
 
1,480
40,700
Сombat radius (km)
277
 
740
7,210
with 1860 kg warload
Dynamic Performance
Rate of climb (m/min)
1.9
 
2,130
36,000
Combat
Guns (qt)
1
 
1
18
.308 in (7.62 mm) GAU-2B/A minigun (mounted in nose)
Missiles (qt)
1
 
-1
24
AIM-9 Sidewinder
Rockets (qt)
1
 
28
76
70 mm/2.75 inch rockets
Bombs weight (kg)
2
 
241
39,000
Stat
Number built (qt)
0
 
577
43,000
Introduction 1967
First flight 1963

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