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    • Year
      1906
      2018
    • Length
      21 m
      33 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      138 m2
      208 m2
    • Wingspan (Beam)
      14 m
      21 m
    • Wing loading
      146 kg/m2
      221 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
      18472 kg
      27710 kg
    • Max. takeoff weight (Gross weight)
      37206 kg
      55810 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
      2552 km/h
      3828 km/h
    • Сruise Speed
      52 km/h
      3087 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
      208 kN/kg
      313 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      148 kN
      224 kN
    • Service ceiling
      19531 m
      29298 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1626 km
      2440 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
      4388 m/min
      6584 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
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      2 qt
      4 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

North American Aviation XF-108 Rapier

TypeAircraft
Company

North American Aviation

Scheme

Concept

High wing

Monoplane

Geometry
Length (m)
1.9
 
27.2
88.7
Height (m)
0.6
 
6.7
50.1
Wings
Wing area (m2)
1.1
 
173.3
925
Wingspan (Beam) (m)
0.1
 
17.5
95
Wing loading (kg/m2)
3.1
 
183.4
829
Weights
Empty weight (kg)
8
 
23,091.0
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
46,508
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
3,190
28,165
Power
Thrust/weight (kN/kg)
0.0
 
0.6
2.1
Afterburning thrust (kN/kg)
29.4
 
260.6
980
2 powerplants 130,3
Thrust (kN)
1.5
 
186
1,914
2 powerplants 93 hp each
Performance
Service ceiling (m)
0.6
 
24,414.5
161,544
Range (Ferry range) (km)
4
 
2,033
40,700
combat
Dynamic Performance
Rate of climb (m/min)
1.9
 
5,486
36,000
Combat
Guns (qt)
1
 
4
18
20 mm cannon
Missiles (qt)
1
 
3
24
Hughes GAR-9A air-to-air missiles in a rotary weapons bay
Stat
Number built (qt)
0
 
1
43,000
Introduction 1959

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