Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      18 m2
      29 m2
    • Wingspan (Beam)
      9 m
      14 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
      2944 kg
      4416 kg
    • Max. takeoff weight (Gross weight)
      4782 kg
      7174 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
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      672 km/h
      1008 km/h
    • Сruise Speed
      536 km/h
      804 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
      0 hp
      60000 hp
    • Thrust
      20 kN
      32 kN
    • Service ceiling
      9851 m
      14777 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1348 km
      2022 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
      1511 m/min
      2268 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
      423 qt
      635 qt
    • Price
      41 USD
      750000000 USD

North American Aviation T-2 Buckeye

TypeAircraft
Company

North American Aviation

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
11.7
88.7
Height (m)
0.6
 
4.5
50.1
Wings
Wing area (m2)
1.1
 
23.7
925
Wingspan (Beam) (m)
0.1
 
11.6
95
Weights
Empty weight (kg)
8
 
3,680
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,977.9
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
840
28,165
at 7600 m
Сruise Speed (km/h)
52
 
670
3,087
Power
Thrust (kN)
1.5
 
26.2
1,914
2 powerplants 13,12 each
Performance
Service ceiling (m)
0.6
 
12,313.9
161,544
Range (Ferry range) (km)
4
 
1,685
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,889.8
36,000
Stat
Number built (qt)
0
 
529
43,000
Introduction 1958
First flight 31.01.1958
Stop production 2008

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