Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      0 m
      95 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
      6 m
      11 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
      1 m
      2 m
    • Empty weight
      439 kg
      659 kg
    • Max. takeoff weight (Gross weight)
      925 kg
      1388 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      453 kg
      681 kg
    • Capacity passengers
      2 per.
      4 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      160 km/h
      240 km/h
    • Сruise Speed
      155 km/h
      233 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
      181 l
      273 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
      187 hp
      282 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2440 m
      3660 m
    • Static ceiling
      4388 m
      5485 m
    • Range (Ferry range)
      472 km
      708 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      2 h
      5 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
      336 m/min
      505 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Schweizer S-333

TypeHelicopter
Company

Schweizer Aircraft

Sikorsky Aircraft Corporation

Geometry
Length (m)
1.9
 
9.5
88.7
Height (m)
0.6
 
3.4
50.1
Rotors
Main rotor diameter (m)
1.2
 
8.2
62
1.2
 
8.4
62
Tail rotor diameter (m)
0.8
 
1.3
4.9
Weights
Empty weight (kg)
8
 
548.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,156.7
575,000
Capacity
Crew (per.)
1
 
2
112
1-2 pilots
Payload (kg)
23
 
567.0
122,470
Capacity passengers (per.)
1
 
3
400
1-3
Speeds
Max. Speed (km/h)
25
 
200
28,165
Сruise Speed (km/h)
52
 
194
3,087
Fuel
Fuel Capacity (l)
23
 
227
320,000
Power
Total Power (hp)
0.4
 
234.6
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
3,050
161,544
Static ceiling (m)
3
 
5,485
5,485
Range (Ferry range) (km)
4
 
590
40,700
Endurance (h)
0.0
 
3.4
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
420.6
36,000
Stat
Introduction 1988
First flight 14.06.1988

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