Difference between revisions of "Template:Aircraft specifications/sandbox/testcases"
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blackwiki>GraemeLeggett (→Specifications (Fairey Rotodyne "Y"): both switch) |
blackwiki>GraemeLeggett (add examples) |
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| − | == | + | ==Helicopter (Wessex HC.2)== |
| + | {{aircraft specifications/sandbox| | ||
| + | <!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> | ||
| + | <!-- please answer the following questions --> | ||
| + | |plane or copter?=copter | ||
| + | |jet or prop?=prop | ||
| + | <!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item doesn't apply, like capacity, leave it blank. For additional lines, end your alt units with )</li> and start a new, fully-formatted line with <li> --> | ||
| + | |crew=Two pilots (civilian type 60 Wessex cleared for single pilot operation in UK) | ||
| + | |capacity=16 troops or 8 stretchers | ||
| + | |length main=65 ft 8 in | ||
| + | |length alt=20.03 m | ||
| + | |span main=56 ft 0 in | ||
| + | |span alt=17.07 m | ||
| + | |height main=16 ft 2 in | ||
| + | |height alt=4.93 m | ||
| + | |area main=2,463 ft² | ||
| + | |area alt=229 m² | ||
| + | |empty weight main=8,304 lb | ||
| + | |empty weight alt=3,767 kg | ||
| + | |loaded weight main=lb | ||
| + | |loaded weight alt= kg | ||
| + | |max takeoff weight main=13,500 lb | ||
| + | |max takeoff weight alt=6,123 kg | ||
| + | |||
| + | |engine (prop)= [[Rolls-Royce Gnome]] | ||
| + | |type of prop= [[turboshaft]] | ||
| + | |number of props= 2 | ||
| + | |power main= 1,535 shp | ||
| + | |power alt= 1,150 kW | ||
| + | |||
| + | |max speed main=133 mph | ||
| + | |max speed alt=212 km/h | ||
| + | |range main= 480 miles | ||
| + | |range alt= 772 km | ||
| + | |ceiling main=10,000 ft | ||
| + | |ceiling alt=3,050 m | ||
| + | |climb rate main=ft/min | ||
| + | |climb rate alt= m/s | ||
| + | |loading main= 5.5 lb/ft² | ||
| + | |loading alt= 26.7 kg/m² | ||
| + | |power/mass main= 0.11 hp/lb | ||
| + | |power/mass alt= 0.19 kW/kg | ||
| + | }} | ||
| + | |||
| + | |||
| + | ==Gyrodyne - wing and rotor ([[Fairey Rotodyne]])== | ||
{{aircraft specifications/sandbox| | {{aircraft specifications/sandbox| | ||
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}} | }} | ||
| − | == | + | ==aircraft with engines ([[Tarrant Tabor]]) == |
{{aircraft specifications/sandbox | {{aircraft specifications/sandbox | ||
<!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> | <!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> | ||
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|jet or prop?=prop | |jet or prop?=prop | ||
| − | |ref= | + | |ref= |
|crew=Six | |crew=Six | ||
| Line 116: | Line 161: | ||
}} | }} | ||
| − | == | + | ==aircraft without engines ([[Göppingen Gö 4]])== |
{{aircraft specifications/sandbox | {{aircraft specifications/sandbox | ||
|ref= | |ref= | ||
| Line 129: | Line 174: | ||
|span alt=48 ft 7 in | |span alt=48 ft 7 in | ||
| − | |||
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| − | |||
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|height main=dunno | |height main=dunno | ||
|height alt= | |height alt= | ||
|wing area main=19 m2 | |wing area main=19 m2 | ||
|wing area alt=204 sq ft | |wing area alt=204 sq ft | ||
| − | + | ||
| − | + | ||
| − | + | |aspect ratio=not given | |
| − | |||
| − | |||
| − | |||
| − | |aspect ratio= | ||
|empty weight main=180 kg | |empty weight main=180 kg | ||
|empty weight alt=400 lb | |empty weight alt=400 lb | ||
|gross weight kg=350 | |gross weight kg=350 | ||
|gross weight lb=770 | |gross weight lb=770 | ||
| − | |||
| − | |||
| − | |max speed | + | |
| − | |max speed | + | |max speed main= |
| − | |max speed | + | |max speed alt= |
| − | + | |max speed more=<!-- supersonic aircraft --> | |
| − | + | ||
| − | |range | + | |range main= |
| − | |range | + | |range alt= |
| − | |endurance | + | |endurance main=<!-- if range unknown --> |
| − | |endurance | + | |endurance alt=<!-- if range unknown --> |
| − | |ceiling | + | |ceiling main= |
| − | |ceiling | + | |ceiling alt= |
| − | |glide ratio= | + | |glide ratio=not given |
| − | |climb rate | + | |climb rate main= |
| − | |climb rate | + | |climb rate alt= |
|sink rate main=<!-- sailplanes -->1.0 m/s | |sink rate main=<!-- sailplanes -->1.0 m/s | ||
|sink rate alt=<!-- sailplanes -->200 ft/min | |sink rate alt=<!-- sailplanes -->200 ft/min | ||
| Line 180: | Line 206: | ||
}} | }} | ||
| − | == | + | ==Aircraft with types of engine ([[Saunders-Roe SR.177]])== |
| + | |||
| + | {{aircraft specifications/sandbox | ||
| + | <!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> | ||
| + | <!-- please answer the following questions --> | ||
| + | |plane or copter?=plane | ||
| + | |jet or prop?=both | ||
| + | |||
| + | <!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item doesn't apply, like capacity, leave it blank. For instructions on using |more general=, |more performance=, |power original=, and |thrust original= see [[Template talk:Aircraft specifications]]. To add a new line, end the old one with a right parenthesis ")", and start a new fully formatted line beginning with * --> | ||
| + | |ref= | ||
| + | |crew= one | ||
| + | |capacity= | ||
| + | |length main= 50 ft | ||
| + | |length alt= 15.2 m | ||
| + | |span main= 30 ft | ||
| + | |span alt= 9.1 m | ||
| + | |height main= 14 ft | ||
| + | |height alt= 4.3 m | ||
| + | |area main= | ||
| + | |area alt= | ||
| + | |airfoil= | ||
| + | |empty weight main= | ||
| + | |empty weight alt= | ||
| + | |loaded weight main= 25,500 lb | ||
| + | |loaded weight alt= 11,570 kg | ||
| + | |useful load main= | ||
| + | |useful load alt= | ||
| + | |max takeoff weight main= | ||
| + | |max takeoff weight alt= | ||
| + | |more general= | ||
| + | |||
| + | |engine (jet)= [[de Havilland Gyron Junior]] | ||
| + | |type of jet= [[turbojet]] | ||
| + | |number of jets= 1 | ||
| + | |thrust main= 8,000 lbf | ||
| + | |thrust alt= 35.6 kN | ||
| + | |thrust original= | ||
| + | |afterburning thrust main= | ||
| + | |afterburning thrust alt= | ||
| + | |||
| + | |engine (prop)= [[de Havilland Spectre]] | ||
| + | |type of prop= liquid fuel rocket | ||
| + | |number of props= 1 | ||
| + | |power main= 8,000 lbf | ||
| + | |power alt= 35.6 kN | ||
| + | |power original= | ||
| + | |||
| + | |max speed main= 1,550 mph | ||
| + | |max speed alt= 2,500 km/h | ||
| + | |max speed more=estimated | ||
| + | |cruise speed main= | ||
| + | |cruise speed alt= | ||
| + | |never exceed speed main= | ||
| + | |never exceed speed alt= | ||
| + | |stall speed main= | ||
| + | |stall speed alt= | ||
| + | |range main= | ||
| + | |range alt= | ||
| + | |ceiling main=67,000 ft | ||
| + | |ceiling alt= 20,500 m | ||
| + | |ceiling more=estimated | ||
| + | |climb rate main= 60,000 ft/min | ||
| + | |climb rate alt= 18,300 m/s | ||
| + | |climb rate more=estimated | ||
| + | |loading main= | ||
| + | |loading alt= | ||
| + | |thrust/weight= | ||
| + | |power/mass main= | ||
| + | |power/mass alt= | ||
| + | |more performance= | ||
| + | |||
| + | |missiles=2 [[de Havilland Firestreak|Firestreak]] air-to-air missiles | ||
| + | |avionics=AI-23 airborne interception [[radar]] | ||
| + | }} | ||
| + | |||
| + | |||
| + | ==airship ([[R101]])== | ||
{{aircraft specifications/sandbox | {{aircraft specifications/sandbox | ||
|ref=not given | |ref=not given | ||
Revision as of 12:45, 21 October 2009
Contents
Helicopter (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
- Maximum speed: 133 mph (212 km/h)
- Range: 480 miles (772 km)
- Service ceiling: 10,000 ft (3,050 m)
- Rate of climb: ft/min (m/s)
- Disc loading: 5.5 lb/ft² (26.7 kg/m²)
- Power/mass: 0.11 hp/lb (0.19 kW/kg)
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
- Maximum speed: 213 mph (343 km/h)
- Range: 520 mi (830 km)
- Wing loading: 5.2 lb/ft² (25 kg/m²)
- Power/mass (prop): 0.17 hp/lb (280 W/kg)
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
- Maximum speed: over 96 knots (110 mph, 177 km/h)
- Endurance: 12 hours
- Service ceiling: 13,000 ft (3,970 m)
- Wing loading: 9.02 lb/ft² (44.1 kg/m²)
- Power/mass: 0.06 hp/lb (0.099 kW/kg)
- Climb to 10,000 ft (3,050 m): 33 min 30 sec
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
- sink rate: 1.0 m/s (200 ft/min)
- Glide ratio: not given
Aircraft with types of engine (Saunders-Roe SR.177)
General characteristics
- Crew: one
- Length: 50 ft (15.2 m)
- Wingspan: 30 ft (9.1 m)
- Height: 14 ft (4.3 m)
- Loaded weight: 25,500 lb (11,570 kg)
- Powerplant:
- 1 × de Havilland Gyron Junior turbojet, 8,000 lbf (35.6 kN)
- 1 × de Havilland Spectre liquid fuel rocket, 8,000 lbf (35.6 kN)
Performance
- Maximum speed: 1,550 mph (2,500 km/h) estimated
- Service ceiling: 67,000 ft (20,500 m) estimated
- Rate of climb: 60,000 ft/min (18,300 m/s) estimated
Armament
- Missiles: 2 Firestreak air-to-air missiles
Avionics
AI-23 airborne interception radar
airship (R101)
Data from not given
General characteristics
- Crew: 45
- Capacity: 100 passengers
- Length: 777 ft (237 m)
- Wingspan: ()
- Height: ()
- Powerplant: 5 × Beardmore Tornado 8 cylinder Diesel, 585 hp (436 kW) each
Performance
- Maximum speed: 71 mpg (114 km/h)