Difference between revisions of "Template:Aircraft specifications/sandbox/testcases"

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blackwiki>GraemeLeggett
(→‎Helicopter (Wessex HC.2): note part empty param)
blackwiki>GraemeLeggett
(update params)
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==Helicopter (Wessex HC.2)==
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==Helicopter ([[Westland Wessex]] HC.2)==
 
{{aircraft specifications/sandbox|
 
{{aircraft specifications/sandbox|
 
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|span main=
 
|span main=
|span ft=
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|span alt=
|span in=
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|diameter alt=40 m
 
|diameter alt=40 m
 
|diameter main=131 ft
 
|diameter main=131 ft
  
|width m=<!-- if applicable -->
 
|width ft=<!-- if applicable -->
 
|width in=<!-- if applicable -->
 
 
|height main=
 
|height main=
 
|height alt=
 
|height alt=
  
|wing area sqm=
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|area main=
|wing area sqft=
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|area alt=
 
|volume alt= 160,000 m3
 
|volume alt= 160,000 m3
 
|volume main=5.5 million cubic feet
 
|volume main=5.5 million cubic feet
|empty weight kg=
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|empty weight main=
|empty weight lb=
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|empty weight alt=
|gross weight kg=
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|gross weight main=
|gross weight lb=
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|gross weight alt=
 
|lift alt=45,000 kg
 
|lift alt=45,000 kg
 
|lift main=100,000 lb
 
|lift main=100,000 lb

Revision as of 12:10, 22 October 2009

Helicopter (Westland Wessex HC.2)

General characteristics

  • Crew: Two pilots (civilian type 60 Wessex cleared for single pilot operation in UK)
  • Capacity: 16 troops or 8 stretchers
  • Length: 65 ft 8 in (20.03 m)
  • Rotor diameter: 56 ft 0 in (17.07 m)
  • Height: 16 ft 2 in (4.93 m)
  • Disc area: 2,463 ft² (229 m²)
  • Empty weight: 8,304 lb (3,767 kg)
  • Loaded weight: ? lb (? kg)
  • Max. takeoff weight: 13,500 lb (6,123 kg)
  • Powerplant: 2 × Rolls-Royce Gnome turboshaft, 1,535 shp (1,150 kW) each

Performance

Gyrodyne - wing and rotor (Fairey Rotodyne)

General characteristics

  • Crew: 2
  • Capacity: 48 passengers
  • Length: 58 ft 8 in (17.9 m)
  • Wingspan: 90 ft 0 in (27.4 m)
  • Height: 22 ft 2 in (6.76 m)
  • Wing area: 6,360 ft² (591 m²)
  • Loaded weight: 33,000 lb (15,000 kg)
  • Max. takeoff weight: 38,000 lb (17,000 kg)
  • Powerplant:
    • 4 × rotor tip jet burning compressed air/fuel, () each
    • 2 × Napier Eland turboprops, 2,800 hp (2,100 kW) each

Performance

aircraft with engines (Tarrant Tabor)

General characteristics

  • Crew: Six
  • Length: 73 ft 2 in (22.31 m)
  • Wingspan: 131 ft 3 in (40.02 m)
  • Height: 37 ft 3 in (11.36 m)
  • Wing area: 4,950 ft² (460 m²)
  • Empty weight: 24,750 lb (11,250 kg)
  • Loaded weight: 44,672 lb (20,305 kg)
  • Powerplant: 6 × Napier Lion 12 cylinder, water cooled broad arrow engines (four tractor, two pusher), 450 hp (336 kW) each

Performance

Armament

  • Bombs: approximately 4,600 lb planned

aircraft without engines (Göppingen Gö 4)

General characteristics

  • Crew: Two, pilot and instructor
  • Length: 6.74 m (22 ft 1 in)
  • Wingspan: 14.8 m (48 ft 7 in)
  • Height: dunno ()
  • Aspect ratio: not given
  • Empty weight: 180 kg (400 lb)

Performance

Aircraft with two types of engine (Saunders-Roe SR.177)

General characteristics

Performance

Armament

Avionics
AI-23 airborne interception radar

airship (R101)

Data from not given

General characteristics

Performance

Everything in (made up)

Data from Someone who wrote a book

General characteristics

  • Crew: 5 (Pilot and 4 other guys)
  • Capacity: lots of stuff
  • Payload: 13 stone (about 70 kg) on a good day
  • Length: 100 ft ()
  • Wingspan: 100 ft ()
  • Height: 20 ft (so many metres)
  • Wing area: 200 sq yards ()
  • Empty weight: 754 kg ()
  • Loaded weight: 1,010 kg (about 500 lb)
  • Max. takeoff weight: 1,500 kg ()
  • Powerplant:
    • 1 × RR Wensum turbjet, 700 lbf ()
    • 2 × Bristol Eros piston thingy, 500 hp () with supercharging each
      • Propellers: big flappy ones rotor, 1 per engine
    • Propeller diameter: 40 ft 6 inches (12.44 metres)

Performance

Armament

  • Guns: 4 Brownings
  • Hardpoints: 2 with a capacity of 100 kg and provisions to carry combinations of:
    • Missiles: Black Cat Roman Candles
  • Rockets: 4 RP3
  • Missiles: none
  • Bombs: 2 x 100 lb MC

Avionics

  • Garmin GPS

Stuff