Search filter

    • Year
      1906
      2018
    • Length
      10 m
      17 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      25 m2
      39 m2
    • Wingspan (Beam)
      10 m
      17 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
      3359 kg
      5039 kg
    • Max. takeoff weight (Gross weight)
      6444 kg
      9667 kg
    • Loaded weight
      5929 kg
      8895 kg
    • Crew
      4 per.
      6 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      5 per.
      9 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      708 km/h
      1062 km/h
    • Сruise Speed
      644 km/h
      966 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
      21 kN
      32 kN
    • Service ceiling
      9760 m
      14640 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3215 km
      4823 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
      640 qt
      960 qt
    • Price
      41 USD
      750000000 USD

North American Aviation Sabreliner

TypeAircraft
Company

North American Aviation

Rockwell International

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
13.4
88.7
Height (m)
0.6
 
4.9
50.1
Wings
Wing area (m2)
1.1
 
31.8
925
Wingspan (Beam) (m)
0.1
 
13.6
95
Weights
Empty weight (kg)
8
 
4,198.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,055.8
575,000
Loaded weight (kg)
5
 
7,412
242,500
Capacity
Crew (per.)
1
 
5
112
4-5
Capacity passengers (per.)
1
 
7
400
5-7 pax.
Speeds
Max. Speed (km/h)
25
 
885
28,165
Сruise Speed (km/h)
52
 
805
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.3
2.1
Thrust (kN)
1.5
 
26.6
1,914
2 powerplants 13,3 kN each
Performance
Service ceiling (m)
0.6
 
12,200
161,544
Range (Ferry range) (km)
4
 
4,018.8
40,700
Stat
Number built (qt)
0
 
800
43,000
Introduction 1958
First flight 16.09.1958

Similar aircraft

Get more

Museums on map

Museums

Comments