Template:Infobox rocket stage
Jump to navigation
Jump to search
File:Test Template Info-Icon - Version (2).svg Template documentation[view] [edit] [history] [purge]
.svg){kind=link}
| File:Lua-Logo.svg | This template uses Lua: |
Usage
Script error: No such module "Parameter names example".
All parameters except engines, thrust, and fuel are optional.
{{Infobox rocket stage
<!-- Image -->
| image = <!--image filename (omit "Image:" prefix)-->
| caption = <!--image caption-->
<!-- Basic information -->
| name = <!--becomes infobox title-->
| manufacturer = <!--stage manufacturer-->
| country = <!--country of origin, do not use flag-->
| rockets = <!--vehicle(s) stage was used on-->
<!-- General characteristics -->
| height = <!--height in meters, use {{convert}}-->
| diameter = <!--diameter in meters, use {{convert}}-->
| mass = <!--gross mass in kilograms, use {{convert}}-->
| propmass = <!--propellant mass in kilograms, use {{convert}}-->
| empty = <!--dry mass in kilograms, use {{convert}}-->
<!-- Associated Stages -->
| family = <!--if a member of a family of stages-->
| derived_from = <!--if derived from another stage or stages-->
| derivatives = <!--if derivative stages-->
| comparable = <!--if any similar, unrelated stage-->
<!-- Launch history -->
| status = <!--active, retired, under development, cancelled, etc-->
| launches = <!--total launches to date-->
| success = <!--number of times stage has operated successfully-->
| fail = <!--number of times stage itself has failed-->
| noburn = <!--lower stage failed-->
| other_outcome = <!--other-->
| first = <!--date of first flight-->
| last = <!--date of last flight-->
| only = <!--date of launch if stage flew only once-->
<!--Engine details (optional)-->
| stagedata = <!--insert one of the following templates for each engine types:-->
{{Infobox rocket/stage
| name =
| engines = <!--number of engines used on the rocket stage-->
| solid = <!--set to "yes" (lowercase) to change Engines to Motor for solid motors-->
| thrust = <!--thrust provided by a single engine in kN, use {{cvt|THRUST|kN}}-->
| SI = <!--specific impulse of an individual engine, in seconds, use {{convert|ISP_IN_SECONDS|isp}}-->
| burntime = <!--burn time-->
| fuel = <!--fuel used in engine-->
}}
}}
Obsolete (legacy) parameters
These parameters are supported by the template to allow it to display properly on articles that have not yet been converted to the new format. They should not be introduced into new articles/transclusions.
| alt-height = <!--height in feet-->
| alt-diameter = <!--diameter in feet-->
| alt-mass = <!--gross mass in pounds-->
| alt-propmass = <!--propellant mass in pounds-->
| alt-thrust = <!--thrust in lbf-->
<!-- Engine details -->
| engines = <!--number and type of engines used stage, required-->
| thrust = <!--thrust provided by stage in kN, use {{convert}}, required-->
| SI = <!--specific impulse of stage in s-->
| time = <!--stage burn time in s -->
| fuel = <!--propellant used in stage, required-->
Example
| File:Ap6-MSFC-6758331.jpg | |
| Manufacturer | North American |
|---|---|
| Country of origin | USA |
| Used on | Saturn V (stage 2) Saturn INT-21 (stage 2) |
| General characteristics | |
| Height | Script error: No such module "convert". |
| Diameter | Script error: No such module "convert". |
| Gross mass | Script error: No such module "convert". |
| Propellant mass | Script error: No such module "convert". |
| Empty mass | Script error: No such module "convert". |
| Launch history | |
| Status | Retired |
| Total launches | 13 |
| Successes (stage only) | 12 |
| Other | Partial failure (Apollo 6) |
| First flight | November 9, 1967 (AS-501) Apollo 4 |
| Last flight | May 14, 1973 (AS-513) Skylab 1 |
| Saturn V S-II | |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 5 Rocketdyne J-2 |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | Script error: No such module "convert". |
| Specific impulse | Script error: No such module "convert". |
| Burn time | 367 s |
| Propellant | LOX/LH2 |
{{Infobox rocket stage
| image = ap6-MSFC-6758331.jpg
| caption = The [[Apollo 6]] S-II stage during stacking operations in the [[Vehicle Assembly Building|VAB]]
| name = S-II
| manufacturer = [[North American Aviation|North American]]
| country = USA
| rockets = [[Saturn V]] (stage 2)<br>[[Saturn INT-21]] (stage 2)
| height = {{convert|24.9|m|abbr=on}}
| diameter = {{convert|10|m|abbr=on}}
| mass = {{convert|1058000|lbs|abbr=on|order=flip}}
| propmass = {{convert|977000|lbs|abbr=on|order=flip}}
| empty = {{convert|79700|lbs|abbr=on|order=flip}}
| status = Retired
| launches = 13
| success = 12
| other_outcome = Partial failure ([[Apollo 6]])
| first = November 9, 1967 (AS-501) [[Apollo 4]]
| last = May 14, 1973 (AS-513) [[Skylab 1]]
| stagedata =
{{Infobox rocket/stage
| name = Saturn V S-II
| engines = 5 [[Rocketdyne J-2]]
| thrust = {{convert|1000000|lbf|kN|abbr=on|order=flip}}
| SI = {{convert|421|isp}}
| burntime = 367 s
| fuel = [[Liquid oxygen|LOX]]/[[Liquid hydrogen|LH<sub>2</sub>]]
}}
}}
Tracking categories
- Category:Pages using infobox rocket stage with unknown parameters (0)
- Category:Rocketry articles with outdated infoboxes (1)
See also
Script error: No such module "Navbox".