Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      19 m2
      30 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
      2331 kg
      3497 kg
    • Max. takeoff weight (Gross weight)
      3084 kg
      4627 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
      4 qt
      8 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      441 km/h
      663 km/h
    • Сruise Speed
      371 km/h
      557 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
      1140 hp
      1710 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8656 m
      12984 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1364 km
      2046 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
      974 m/min
      1462 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
      1558 qt
      2338 qt
    • Price
      41 USD
      750000000 USD

North American Aviation T-28 Trojan

TypeAircraft
Company

North American Aviation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
10.1
88.7
Height (m)
0.6
 
3.9
50.1
Wings
Wing area (m2)
1.1
 
24.9
925
Wingspan (Beam) (m)
0.1
 
12.2
95
Weights
Empty weight (kg)
8
 
2,913.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,855.5
575,000
Capacity
Crew (per.)
1
 
2
112
Hardpoints (qt)
1
 
6
2,576
Speeds
Max. Speed (km/h)
25
 
552
28,165
Сruise Speed (km/h)
52
 
464
3,087
Power
Total Power (hp)
0.4
 
1,425
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
10,820
161,544
Range (Ferry range) (km)
4
 
1,705
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,218
36,000
Stat
Number built (qt)
0
 
1,948
43,000
Introduction 1949
First flight 24.09.1949
Stop production 1994

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