Difference between revisions of "Template:Airspec-imp"
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↑ {{cite {type of source}|author|title|year|etc}}
↑ {{cite {type of source}|author|title|year|etc}}
blackwiki>Karl Dickman (fix redirect) |
blackwiki>Karl Dickman (update to changes in the template) |
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|ref={name of source}<ref>{{cite {type of source}|author|title|year|etc}}</ref> {name of source}<ref>{{cite {type of source}|author|title|year|etc}}</ref>. | |ref={name of source}<ref>{{cite {type of source}|author|title|year|etc}}</ref> {name of source}<ref>{{cite {type of source}|author|title|year|etc}}</ref>. | ||
| − | <!-- 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: | + | <!-- 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 * --> |
|crew= | |crew= | ||
|capacity= | |capacity= | ||
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|power original= | |power original= | ||
| − | |max speed main= | + | |max speed main= knots |
| − | |max speed alt= km/h | + | |max speed alt= mph, km/h |
| − | |cruise speed main= | + | |cruise speed main= knots |
| − | |cruise speed alt= km/h | + | |cruise speed alt= mph, km/h |
| − | |never exceed speed main= | + | |never exceed speed main= knots |
| − | |never exceed speed alt= km/h | + | |never exceed speed alt= mph, km/h |
| − | |stall speed main= | + | |stall speed main= knots |
| − | |stall speed alt= km/h | + | |stall speed alt= mph, km/h |
| − | |range main= | + | |range main= nm |
| − | |range alt= km | + | |range alt= mi, km |
|ceiling main= ft | |ceiling main= ft | ||
|ceiling alt= m | |ceiling alt= m | ||
| Line 62: | Line 62: | ||
|thrust/weight=<!-- a unitless ratio --> | |thrust/weight=<!-- a unitless ratio --> | ||
|power/mass main= hp/lb | |power/mass main= hp/lb | ||
| − | |power/mass alt= | + | |power/mass alt= W/kg |
|more performance= | |more performance= | ||
| − | |armament= | + | |armament= |
|avionics= | |avionics= | ||
}} | }} | ||
Revision as of 23:41, 9 May 2006
Specifications ()
Data from {name of source}[1] {name of source}[2].
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)