Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      14 m2
      22 m2
    • Wingspan (Beam)
      9 m
      15 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
      1199 kg
      1799 kg
    • Max. takeoff weight (Gross weight)
      1868 kg
      2804 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
      4 per.
      6 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      320 km/h
      480 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      92 km/h
      138 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
      6096 m
      9144 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1512 km
      2270 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
      360 m/min
      542 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
      252 qt
      378 qt
    • Price
      41 USD
      750000000 USD

Cessna T303 Crusader

TypeAircraft
Company

Cessna Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
9.3
88.7
Height (m)
0.6
 
4.1
50.1
Wings
Wing area (m2)
1.1
 
17.6
925
1.1
 
17.6
925
Wingspan (Beam) (m)
0.1
 
11.9
95
Weights
Empty weight (kg)
8
 
1,499.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,336
575,000
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
5
400
Speeds
Max. Speed (km/h)
25
 
400
28,165
at 5485 m
Stall Speed (km/h)
40
 
115
257.7
flaps down, power off
40
 
115
257.7
flaps down, power off
Power
Total Power (hp)
0.4
 
500
60,000
2 powerplants 250 hp each
Performance
Service ceiling (m)
0.6
 
7,620
161,544
Range (Ferry range) (km)
4
 
1,891
40,700
econ cruise at 3050 m
Dynamic Performance
Rate of climb (m/min)
1.9
 
451.1
36,000
Stat
Number built (qt)
0
 
315
43,000
First flight 14.02.1978

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