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
      21 m2
      33 m2
    • Wingspan (Beam)
      10 m
      16 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
      1270 kg
      1906 kg
    • Max. takeoff weight (Gross weight)
      2199 kg
      3300 kg
    • Loaded weight
      2068 kg
      3103 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
      251 km/h
      377 km/h
    • Сruise Speed
      225 km/h
      338 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
      392 hp
      588 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5364 m
      8046 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      965 km
      1449 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
      1 m/min
      36000 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
      4320 qt
      6480 qt
    • Price
      41 USD
      750000000 USD

Cessna AT-17 Bobcat

TypeAircraft
Company

Cessna Aircraft Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
10.0
88.7
Height (m)
0.6
 
3.0
50.1
Wings
Wing area (m2)
1.1
 
27.4
925
Wingspan (Beam) (m)
0.1
 
12.8
95
Weights
Empty weight (kg)
8
 
1,587.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,749.7
575,000
Loaded weight (kg)
5
 
2,585.5
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
313.8
28,165
Сruise Speed (km/h)
52
 
281.6
3,087
Power
Total Power (hp)
0.4
 
490
60,000
2 powerplants 245 hp each
Performance
Service ceiling (m)
0.6
 
6,705
161,544
Range (Ferry range) (km)
4
 
1,207
40,700
Stat
Number built (qt)
0
 
5,400
43,000
Introduction 1939
First flight 26.03.1939

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