Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      15 m2
      24 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
      2017 kg
      3027 kg
    • Max. takeoff weight (Gross weight)
      3137 kg
      4706 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      1153 kg
      1731 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
      621 km/h
      933 km/h
    • Сruise Speed
      504 km/h
      756 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      10 kN
      16 kN
    • Service ceiling
      9997 m
      14997 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1728 km
      2594 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      758 m
      1138 m
    • Landing roll
      583 m
      875 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      733 m/min
      1101 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
      340 qt
      510 qt
    • Price
      2624000 USD
      3936000 USD

Cessna Citation Mustang

TypeAircraft
Company

Cessna Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
12.4
88.7
Height (m)
0.6
 
4.1
50.1
Wings
Wing area (m2)
1.1
 
19.5
925
Wingspan (Beam) (m)
0.1
 
13.2
95
Weights
Empty weight (kg)
8
 
2,522.0
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,921.3
575,000
Capacity
Crew (per.)
1
 
1
112
1 or 2 pilots
Useful load (kg)
26.4
 
1,442
90,700
Capacity passengers (per.)
1
 
5
400
Speeds
Max. Speed (km/h)
25
 
777
28,165
Сruise Speed (km/h)
52
 
630
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.3
2.1
at max. takeoff weight
Thrust (kN)
1.5
 
13.0
1,914
2 powerplants 6,49 kN each
Performance
Service ceiling (m)
0.6
 
12,496.8
161,544
Range (Ferry range) (km)
4
 
2,161
40,700
at max. takeoff weight
Takeoff roll (m)
20
 
948
3,200
Landing roll (m)
20
 
729
2,570
Dynamic Performance
Rate of climb (m/min)
1.9
 
917
36,000
Stat
Number built (qt)
0
 
425
43,000
Price (USD)
41.5
 
3.3 million
750.0 million
Introduction 2005
First flight 23.04.2005

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