Difference between revisions of "Template:Airspec-imp"
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blackwiki>Mike Peel (Categorize into Category:Aviation templates using AWB) |
blackwiki>GraemeLeggett (update) |
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| Line 57: | Line 57: | ||
|power original= | |power original= | ||
| + | |propeller or rotor?=<!-- options: propelller/rotor --> | ||
| + | |propellers= | ||
| + | |number of propellers per engine= | ||
| + | |propeller diameter main= | ||
| + | |propeller diameter alt= | ||
| + | |||
|max speed main= knots | |max speed main= knots | ||
|max speed alt= mph, km/h | |max speed alt= mph, km/h | ||
| Line 67: | Line 73: | ||
|range main= nm | |range main= nm | ||
|range alt= mi, km | |range alt= mi, km | ||
| + | |ferry range main= | ||
| + | |ferry range alt= | ||
| + | |ferry range more= | ||
|ceiling main= ft | |ceiling main= ft | ||
|ceiling alt= m | |ceiling alt= m | ||
| Line 78: | Line 87: | ||
|more performance= | |more performance= | ||
| − | |armament= | + | |armament=<!-- if you want to use the following specific parameters, do not use this line at all--> |
| + | |guns= | ||
| + | |bombs= | ||
| + | |rockets= | ||
| + | |missiles= | ||
| + | |hardpoints= | ||
| + | |hardpoint capacity= | ||
|avionics= | |avionics= | ||
Revision as of 12:02, 11 September 2007
Do not insert figures into this template. This template is only to be inserted into the page you are editing by using the command {{subst:airspec-imp}} and saving the page. The contents will appear next time you edit the page. If you do not understand how to use this template, please ask at Wikipedia talk:WikiProject Aircraft
Specifications ()
Data from {name of first source}[1]
General characteristics
- Length: ft in (m)
- Wingspan: ft in (m)
- Height: ft in (m)
- Wing area: ft² (m²)
- Empty weight: lb (kg)
- Useful load: lb (kg)
- Loaded weight: lb (kg)
- Max. takeoff weight: lb (kg)
Performance
- Maximum speed: knots (mph, km/h)
- Cruise speed: knots (mph, km/h)
- Stall speed: knots (mph, km/h)
- Never exceed speed: knots (mph, km/h)
- Range: nm (mi, km)
- Service ceiling: ft (m)
- Rate of climb: ft/min (m/s)
- Wing loading: lb/ft² (kg/m²)