Difference between revisions of "Template:Airspec-imp"
Jump to navigation
Jump to search
blackwiki>RossPatterson (This template is often used to produce articles with broken {{cite web}} usage, so let's "fix" it here.) |
blackwiki>GraemeLeggett (cleanup params) |
||
| Line 23: | Line 23: | ||
|crew= | |crew= | ||
|capacity= | |capacity= | ||
| + | |payload main= | ||
| + | |payload alt= | ||
| + | |payload more= | ||
| + | |||
|length main= ft in | |length main= ft in | ||
|length alt= m | |length alt= m | ||
| Line 50: | Line 54: | ||
|afterburning thrust main= lbf | |afterburning thrust main= lbf | ||
|afterburning thrust alt= kN | |afterburning thrust alt= kN | ||
| + | |||
|engine (prop)= | |engine (prop)= | ||
|type of prop= | |type of prop= | ||
| Line 57: | Line 62: | ||
|power original= | |power original= | ||
| − | |propeller or rotor?=<!-- options: | + | |propeller or rotor?=<!-- options: propeller/rotor --> |
| − | |propellers= | + | |propellers=<!-- eg the manufacturer or number of blades --> |
|number of propellers per engine= | |number of propellers per engine= | ||
|propeller diameter main= | |propeller diameter main= | ||
| Line 65: | Line 70: | ||
|max speed main= knots | |max speed main= knots | ||
|max speed alt= mph, km/h | |max speed alt= mph, km/h | ||
| + | |max speed more= | ||
|cruise speed main= knots | |cruise speed main= knots | ||
|cruise speed alt= mph, km/h | |cruise speed alt= mph, km/h | ||
| + | |cruise speed more= | ||
|never exceed speed main= knots | |never exceed speed main= knots | ||
|never exceed speed alt= mph, km/h | |never exceed speed alt= mph, km/h | ||
| Line 73: | Line 80: | ||
|range main= nm | |range main= nm | ||
|range alt= mi, km | |range alt= mi, km | ||
| + | |range more= | ||
|ferry range main= | |ferry range main= | ||
|ferry range alt= | |ferry range alt= | ||
| Line 78: | Line 86: | ||
|ceiling main= ft | |ceiling main= ft | ||
|ceiling alt= m | |ceiling alt= m | ||
| + | |celing more= | ||
|climb rate main= ft/min | |climb rate main= ft/min | ||
|climb rate alt= m/s | |climb rate alt= m/s | ||
| + | |climb rate more= | ||
|loading main= lb/ft² | |loading main= lb/ft² | ||
|loading alt= kg/m² | |loading alt= kg/m² | ||
Revision as of 11:45, 21 May 2008
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)