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    • Year
      1906
      2018
    • Length
      17 m
      27 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      38 m2
      58 m2
    • Wingspan (Beam)
      15 m
      24 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      6
      10
    • 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
      7838 kg
      11758 kg
    • Max. takeoff weight (Gross weight)
      12954 kg
      19432 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      9 per.
      15 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      792 km/h
      1190 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
      5832 l
      8750 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
      45 kN
      69 kN
    • Service ceiling
      12435 m
      18654 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4764 km
      7148 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
      890 m/min
      1336 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
      264 qt
      396 qt
    • Price
      18340000 USD
      27510000 USD

Cessna 750

TypeAircraft
Company

Cessna Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
22.1
88.7
Height (m)
0.6
 
5.8
50.1
Wings
Wing area (m2)
1.1
 
48
925
Wingspan (Beam) (m)
0.1
 
19.4
95
Aspect ratio
1.7
 
7.8
25.6
Weights
Empty weight (kg)
8
 
9,797.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
16,193.3
575,000
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
12
400
Speeds
Сruise Speed (km/h)
52
 
991
3,087
at 10700 m
Fuel
Fuel Capacity (l)
23
 
7,291
320,000
Power
Thrust (kN)
1.5
 
57.3
1,914
2 powerplant 28,66 kN each
Performance
Service ceiling (m)
0.6
 
15,544.8
161,544
Range (Ferry range) (km)
4
 
5,956.0
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,112.5
36,000
Stat
Number built (qt)
0
 
330
43,000
Price (USD)
41.5
 
22.9 million
750.0 million
Introduction 1993
First flight 21.12.1993

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