Template:Infobox rocket/doc

Usage

{{{name}}}

[[File:{{{logo}}}|frameless|alt={{{logo_alt}}}|upright={{{logo_upright}}}|{{{logo_alt}}}]]
[[File:{{{image}}}|frameless|alt={{{alt}}}|upright={{{upright}}}|{{{alt}}}]] {{{caption}}}
Function	{{{function}}}
Manufacturer	{{{manufacturer}}}
Country of origin	{{{country-origin}}}
Project cost	{{{pcost}}}
Cost per launch	{{{cpl}}} ({{{alt-cpl}}})
Cost per year	{{{cpl-year}}}
Size
Height	{{{height}}} ({{{alt-height}}})
Diameter	{{{diameter}}} ({{{alt-diameter}}})
Width	{{{width}}} ({{{alt-width}}})
Mass	{{{mass}}} ({{{alt-mass}}})
Stages	{{{stages}}}
Capacity {{{capacities}}}
Payload to LEO	{{{LEO-payload}}} ({{{alt-LEO}}})
Payload to {{{payload-location}}}	{{{payload}}} ({{{alt-payload}}})
Payload to {{{payload2-location}}}	{{{payload2}}} ({{{alt-payload2}}})
Payload to {{{payload3-location}}}	{{{payload3}}} ({{{alt-payload3}}})
Payload to {{{payload4-location}}}	{{{payload4}}} ({{{alt-payload4}}})
Payload to {{{payload5-location}}}	{{{payload5}}} ({{{alt-payload5}}})
Associated rockets
Family	{{{family}}}
Derivatives	{{{derivatives}}}
Comparable	{{{comparable}}}
Launch history
Status	{{{status}}}
Launch sites	{{{sites}}}
Total launches	{{{launches}}}
Successes	{{{success}}}
Failures	{{{fail}}}
Partial failures	{{{partial}}}
Other	{{{other_outcome}}}
Landings	{{{landings}}}
First flight	{{{first}}}
Last flight	{{{last}}}
Launch date	{{{only}}}
Notable payloads	{{{payloads}}}
{{{stagedata}}}Boosters ({{{diff}}}) - {{{boostername}}}
No. boosters	{{{boosters}}}
Engines	{{{boosterengines}}}
Thrust	{{{boosterthrust}}} ({{{alt-boosterthrust}}})
Total thrust	{{{boosterTT}}} ({{{alt-boosterTT}}})
Specific impulse	{{{boosterSI}}}
Burn time	{{{boostertime}}}
Propellant	{{{boosterfuel}}}
Boosters ({{{alt-diff}}}) - {{{alt-boostername}}}
No. boosters	{{{alt-boosters}}}
Engines	{{{alt-boosterengines}}}
Thrust	{{{alt-boostersthrust}}} ({{{alt-alt-boosterthrust}}})
Specific impulse	{{{alt-boosterSI}}}
Burn time	{{{alt-boostertime}}}
Propellant	{{{alt-boosterfuel}}}
Boosters ({{{alt2-diff}}}) {{{alt2-boostername}}}
No. boosters	{{{alt2-boosters}}}
Engines	{{{alt2-boosterengines}}}
Thrust	{{{alt2-boostersthrust}}} ({{{alt2-alt-boosterthrust}}})
Specific impulse	{{{alt2-boosterSI}}}
Burn time	{{{alt2-boostertime}}}
Propellant	{{{alt2-boosterfuel}}}
First stage ({{{stage1diff}}}) - {{{stage1name}}}
Engines	{{{stage1engines}}}
Thrust	{{{stage1thrust}}} ({{{alt-stage1thrust}}})
Specific impulse	{{{stage1SI}}}
Burn time	{{{stage1time}}}
Propellant	{{{stage1fuel}}}
Fuel & Oxidizer mass/volume	{{{stage1fueloxidizermassvolume}}}
First stage ({{{stage1adiff}}}) - {{{stage1aname}}}
Engines	{{{stage1aengines}}}
Thrust	{{{stage1athrust}}} ({{{alt-stage1athrust}}})
Specific impulse	{{{stage1aSI}}}
Burn time	{{{stage1atime}}}
Propellant	{{{stage1afuel}}}
Fuel & Oxidizer mass/volume	{{{stage1afueloxidizermassvolume}}}
Second stage ({{{stage2diff}}}) {{{stage2name}}}
Engines	{{{stage2engines}}}
Thrust	{{{stage2thrust}}} ({{{alt-stage2thrust}}})
Specific impulse	{{{stage2SI}}}
Burn time	{{{stage2time}}}
Propellant	{{{stage2fuel}}}
Second stage ({{{stage2adiff}}}) - {{{stage2aname}}}
Engines	{{{stage2aengines}}}
Thrust	{{{stage2athrust}}} ({{{alt-stage2athrust}}})
Specific impulse	{{{stage2aSI}}}
Burn time	{{{stage2atime}}}
Propellant	{{{stage2afuel}}}
Third stage ({{{stage3diff}}}) - {{{stage3name}}}
Engines	{{{stage3engines}}}
Thrust	{{{stage3thrust}}} ({{{alt-stage3thrust}}})
Specific impulse	{{{stage3SI}}}
Burn time	{{{stage3time}}}
Propellant	{{{stage3fuel}}}
Third stage ({{{stage3adiff}}}) - {{{stage3aname}}}
Engines	{{{stage3aengines}}}
Thrust	{{{stage3athrust}}} ({{{alt-stage3athrust}}})
Specific impulse	{{{stage3aSI}}}
Burn time	{{{stage3atime}}}
Propellant	{{{stage3afuel}}}
Fourth stage ({{{stage4diff}}}) - {{{stage4name}}}
Engines	{{{stage4engines}}}
Thrust	{{{stage4thrust}}} ({{{alt-stage4thrust}}})
Specific impulse	{{{stage4SI}}}
Burn time	{{{stage4time}}}
Propellant	{{{stage4fuel}}}
Fifth stage - {{{stage5name}}}
Engines	{{{stage5engines}}}
Thrust	{{{stage5thrust}}} ({{{alt-stage5thrust}}})
Specific impulse	{{{stage5SI}}}
Burn time	{{{stage5time}}}
Propellant	{{{stage5fuel}}}
Sixth stage - {{{stage6name}}}
Engines	{{{stage6engines}}}
Thrust	{{{stage6thrust}}} ({{{alt-stage6thrust}}})
Specific impulse	{{{stage6SI}}}
Burn time	{{{stage6time}}}
Propellant	{{{stage6fuel}}}

{{Infobox rocket

<!----Image and logos (optional)---->
|logo         =  <!--logo filename (omit "Image:" prefix), required-->
|logo_upright =  <!--logo filesize, e.g. "1" = normal width, "2" = double width, "0.5" = half width, optional-->
|image        =  <!--image filename (omit "Image:" prefix), required-->
|upright      =  <!--reduce width of portrait image to reduce overall infobox length, input "yes" to activate, optional-->
|caption      =  <!--caption, optional-->

<!----Core parameters (required)---->
|name           =  <!--Name(s) of the rocket, optional, defaults to page title-->
|function       =  <!--Purpose of the rocket, required-->
|manufacturer   =  <!--Manufacturer, required-->
|country-origin =  <!--country of origin, optional-->

<!----Costs (optional)---->
|pcost    =  <!--project cost, optional-->
|cpl      =  <!--cost per launch, optional-->
|alt-cpl  =  <!--cost in alternative currency, optional-->
|cpl-year =  <!--year of stated cost per launch-->

<!----Dimensions (required)---->
|height       =  <!--height of the rocket in metres, use {{cvt|HEIGHT|m}}, required-->
|diameter     =  <!--core diameter in metres, use {{cvt|DIAMETER|m}}, required-->
|width        =  <!--width if not axisymmetric, use {{cvt|WIDTH|m}}, optional-->
|mass         =  <!--mass of rocket in kilograms, use {{cvt|MASS|kg}}, required-->
|stages       =  <!--number of stages, not including boosters-->

<!----Payloads (optional)---->
|capacities =  <!--insert one of the following templates for each payload:-->
  {{Infobox rocket/payload
  |location =  <!--Target orbit/trajectory, required. Please use [[Geostationary transfer orbit|GTO]] or [[Low Earth orbit|LEO]] instead of just [[GTO]] or [[LEO]].-->
  |altitude =  <!--Altitude of the target orbit/trajectory in kilometres, use {{cvt|PAYLOAD|km}}, required-->
  |inclination =  <!--Inclination of the target orbit/trajectory in degrees, required-->
  |mass    =  <!--Payload mass in kilograms, use {{cvt|PAYLOAD|kg}}, required-->
  |volume  =  <!--Payload volume in cubic metres, use {{cvt|PAYLOAD|m}}, optional-->
  }}

<!----Associated rockets (optional)---->
|family      =  <!--rocket family, optional-->
|derived_from =  <!--rocket from which this rocket is derived, optional-->
|derivatives =  <!--derived rockets, optional-->
|comparable  =  <!--similar, unrelated rockets, optional-->

<!----Launch history (required)---->
|status   =  <!--current status (eg. Active, Retired, etc), required-->
|sites    =  <!--launch centres and pads, required-->
|launches =  <!--total launches to date, optional-->
|success  =  <!--total successful launches, optional-->
|fail     =  <!--total failed launches, optional-->
|partial  =  <!--total number of launches resulting in partial failure (e.g. incorrect orbit but still usable), optional-->
|other_outcome =  <!--number of launches with unknown outcomes (or in progress), optional-->
|landings =  <!--total number of landings, optional-->
|first    =  <!--date of first flight, optional-->
|last     =  <!--date of latest or final flight, optional-->
|only     =  <!--launch date if only one was launched, optional-->
|payloads =  <!--notable payloads, optional-->

<!--Stages/boosters (optional)-->
|stagedata    =  <!--insert one of the following templates for each stage:-->

  {{Infobox rocket/stage
  |type       =  <!--booster or stage (must be in lower case)-->
  |diff       =  <!--variant of rocket this is used on, optional-->
  |stageno    =  <!--position of stage in rocket, spelled out (eg. First, Second, etc), required if type = stage-->
  |name       =  <!--name of the stage/booster, optional-->
  |number     =  <!--number of boosters, required if type = booster-->
  |length     =  <!--length of a single booster/stage in metres, use {{cvt|LENGTH|m}}, optional-->
  |diameter   =  <!--diameter of a single booster/stage in metres, use {{cvt|DIAMETER|m}}, optional-->
  |width      =  <!--width of a single booster/stage if not axisymmetric, use {{cvt|WIDTH|m}}, optional-->
  |empty      =  <!--empty mass of a single booster/stage in kilograms, use {{cvt|EMPTYMASS|kg}}, optional-->
  |gross      =  <!--gross (fuelled) mass of a single booster/stage, use {{cvt|GROSSMASS|kg}}, optional--> 
  |propmass   =  <!--propellant mass carried by a single booster/stage in kilograms, use {{cvt|PROPMASS|kg}}, optional--> 
  |engines    =  <!--number and type of engines used on each individual booster/stage, required-->
  |solid      =  <!--set to "yes" (lowercase) to change Engines to Motor for solid motors-->
  |thrust     =  <!--thrust provided by a single booster/stage in kN, use {{cvt|THRUST|kN}}, required-->
  |total      =  <!--total thrust for all boosters in kN, use {{cvt|THRUST|kN}}, optional-->
  |SI         =  <!--specific impulse of an individual booster/stage, in seconds, use {{convert|ISP_IN_SECONDS|isp}}, optional-->
  |burntime   =  <!--burn time, required-->
  |fuel       =  <!--propellant (include fuel and oxidizer) used in stage/boosters, required-->
  }}

}}

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.

<!--LEO payload (optional)-->
|LEO-payload =  <!--Payload mass in kilograms to a typical Low Earth orbit, optional-->
|alt-LEO     =  <!--Payload mass in pounds to a typical Low Earth orbit, optional-->
<!--Specific payload 1, obsolete-->
|payload-location  =  <!--Target orbit/trajectory, required-->
|payload           =  <!--Payload mass in kilograms, required-->
|alt-payload       =  <!--Payload mass in pounds, optional-->
<!--Specific payload 2, obsolete-->
|payload2-location =  <!--Target orbit/trajectory, required-->
|payload2          =  <!--Payload mass in kilograms, required-->
|alt-payload2      =  <!--Payload mass in pounds, optional-->
<!--Specific payload 3, obsolete-->
|payload3-location =  <!--Target orbit/trajectory, required-->
|payload3          =  <!--Payload mass in kilograms, required-->
|alt-payload3      =  <!--Payload mass in pounds, optional-->
<!--Specific payload 4, obsolete-->
|payload4-location =  <!--Target orbit/trajectory, required-->
|payload4          =  <!--Payload mass in kilograms, required-->
|alt-payload4      =  <!--Payload mass in pounds, optional-->
<!--Specific payload 5, obsolete-->
|payload5-location =  <!--Target orbit/trajectory, required-->
|payload5          =  <!--Payload mass in kilograms, required-->
|alt-payload5      =  <!--Payload mass in pounds, optional-->


<!--First booster rockets, obsolete (use stagedata above)-->
|diff           =  <!--variant of rocket these are used on, optional-->
|boostername    =  <!--name of booster rockets, optional-->
|boosters       =  <--number of booster rockets present, required-->
|boosterengines =  <!--number and type of engines used on an individual booster, required-->
|boosterthrust  =  <!--thrust provided by a single booster in kN, required-->
|alt-boosterthurst = <!--thrust provided by a single booster in pounds-force, optional-->
|boosterTT      =  <!--total thrust for all boosters in kN, optional-->
|alt-boosterTT  =  <!--total thrust for all boosters in pounds-force, optional-->
|boosterSI      =  <!--specific impulse of an individual booster, in seconds, optional-->
|boostertime    =  <!--burn time, required-->
|boosterfuel    =  <!--propellant used in boosters, required-->
<!--Second booster rockets, obsolete (use stagedata above)-->
|alt-diff            =  <!--variant of rocket these are used on, optional-->
|alt-boostername     =  <!--name of booster rockets, optional-->
|alt-boosters        =  <--number of booster rockets present, required-->
|alt-boosterengines  =  <!--number and type of engines used on an individual booster, required-->
|alt-boosterthrust   =  <!-thrust provided by a single booster in kN, required-->
|alt-alt-boosterthurst =  <!--thrust provided by a single booster in pounds-force, optional-->
|alt-boosterSI       =  <!--specific impulse of an individual booster, in seconds, optional-->
|alt-boostertime     =  <!--burn time, required-->
|alt-boosterfuel     =  <!--propellant used in boosters, required-->
<!--Third booster rockets, obsolete (use stagedata above)-->
|alt2-diff           =  <!--variant of rocket these are used on, optional-->
|alt2-boostername    =  <!--name of booster rockets, optional-->
|alt2-boosters       =  <--number of booster rockets present, required-->
|alt2-boosterengines =  <!--number and type of engines used on an individual booster, required-->
|alt2-boosterthrust  =  <!-thrust provided by a single booster in kN, required-->
|alt2-alt-boosterthurst =  <!--thrust provided by a single booster in pounds-force, optional-->
|alt2-boosterSI      =  <!--specific impulse of an individual booster, in seconds, optional-->
|alt2-boostertime    =  <!--burn time, required-->
|alt2-boosterfuel    =  <!--propellant used in boosters, required-->
<!--First stage, obsolete (use stagedata above)-->
|stage1diff     =  <!--variant of rocket, optional-->
|stage1name     =  <!--name of stage, optional-->
|stage1engines  =  <!--number and type of engines used on stage, required-->
|stage1thrust   =  <!-thrust provided by stage in kN, required-->
|alt-stage1thurst =  <!--thrust provided by stage in pounds-force, optional-->
|stage1SI       =  <!--specific impulse of stage, in seconds, optional-->
|stage1time     =  <!--burn time, required-->
|stage1fuel     =  <!--propellant used in stage, required-->
|stage1fueloxidizermassvolume =  <!--fuel and oxidizer mass and volume of stage, in tons and m³, optional-->
<!--Alternative first stage, obsolete (use stagedata above)-->
|stage1adiff    =  <!--variant of rocket, optional-->
|stage1aname    =  <!--name of stage, optional-->
|stage1aengines =  <!--number and type of engines used on stage, required-->
|stage1athrust  =  <!-thrust provided by stage in kN, required-->
|alt-stage1athurst =  <!--thrust provided by stage in pounds-force, optional-->
|stage1aSI      =  <!--specific impulse of stage, in seconds, optional-->
|stage1atime    =  <!--burn time, required-->
|stage1afuel    =  <!--propellant used in stage, required-->
|stage1afueloxidizermassvolume =  <!--fuel and oxidizer mass and volume of stage, in tons and m³, optional-->
<!--Second stage, obsolete (use stagedata above)-->
|stage2diff     =  <!--variant of rocket, optional-->
|stage2name     =  <!--name of stage, optional-->
|stage2engines  =  <!--number and type of engines used on stage, required-->
|stage2thrust   =  <!-thrust provided by stage in kN, required-->
|alt-stage2thurst =  <!--thrust provided by stage in pounds-force, optional-->
|stage2SI       =  <!--specific impulse of stage, in seconds, optional-->
|stage2time     =  <!--burn time, required-->
|stage2fuel     =  <!--propellant used in stage, required-->
<!--Alternative second stage, obsolete, use stagedata-->
|stage2adiff    =  <!--variant of rocket, optional-->
|stage2aname    =  <!--name of stage, optional-->
|stage2aengines =  <!--number and type of engines used on stage, required-->
|stage2athrust  =  <!-thrust provided by stage in kN, required-->
|alt-stage2athurst =  <!--thrust provided by stage in pounds-force, optional-->
|stage2aSI      =  <!--specific impulse of stage, in seconds, optional-->
|stage2atime    =  <!--burn time, required-->
|stage2afuel    =  <!--propellant used in stage, required-->
<!--Third stage, obsolete, use stagedata-->
|stage3diff     =  <!--variant of rocket, optional-->
|stage3name     =  <!--name of stage, optional-->
|stage3engines  =  <!--number and type of engines used on stage, required-->
|stage3thrust   =  <!-thrust provided by stage in kN, required-->
|alt-stage3thurst =  <!--thrust provided by stage in pounds-force, optional-->
|stage3SI       =  <!--specific impulse of stage, in seconds, optional-->
|stage3time     =  <!--burn time, required-->
|stage3fuel     =  <!--propellant used in stage, required-->
<!--Alternative third stage, obsolete, use stagedata-->
|stage3adiff    =  <!--variant of rocket, optional-->
|stage3aname    =  <!--name of stage, optional-->
|stage3aengines =  <!--number and type of engines used on stage, required-->
|stage3athrust  =  <!-thrust provided by stage in kN, required-->
|alt-stage3athurst =  <!--thrust provided by stage in pounds-force, optional-->
|stage3aSI      =  <!--specific impulse of stage, in seconds, optional-->
|stage3atime    =  <!--burn time, required-->
|stage3afuel    =  <!--fuel used in stage, required-->
<!--Fourth stage, obsolete, use stagedata-->
|stage4diff     =  <!--variant of rocket, optional-->
|stage4name     =  <!--name of stage, optional-->
|stage4engines  =  <!--number and type of engines used on stage, required-->
|stage4thrust   =  <!-thrust provided by stage in kN, required-->
|alt-stage4thurst =  <!--thrust provided by stage in pounds-force, optional-->
|stage4SI       =  <!--specific impulse of stage, in seconds, optional-->
|stage4time     =  <!--burn time, required-->
|stage4fuel     =  <!--propellant used in stage, required-->
<!--Fifth stage, obsolete, use stagedata-->
|stage5diff     =  <!--variant of rocket, optional-->
|stage5name     =  <!--name of stage, optional-->
|stage5engines  =  <!--number and type of engines used on stage, required-->
|stage5thrust   =  <!-thrust provided by stage in kN, required-->
|alt-stage5thurst =  <!--thrust provided by stage in pounds-force, optional-->
|stage5SI       =  <!--specific impulse of stage, in seconds, optional-->
|stage5time     =  <!--burn time, required-->
|stage5fuel     =  <!--propellant used in stage, required-->
<!--Sixth stage, obsolete, use stagedata-->
|stage6diff     =  <!--variant of rocket, optional-->
|stage6name     =  <!--name of stage, optional-->
|stage6engines  =  <!--number and type of engines used on stage, required-->
|stage6thrust   =  <!-thrust provided by stage in kN, required-->
|alt-stage6thurst =  <!--thrust provided by stage in pounds-force, optional-->
|stage6SI       =  <!--specific impulse of stage, in seconds, optional-->
|stage6time     =  <!--burn time, required-->
|stage6fuel     =  <!--propellant used in stage, required-->


|alt-height   =  <!--height of the rocket in feet, optional-->
|alt-diameter =  <!--core diameter in feet, optional-->
|alt-mass     =  <!--mass of rocket in pounds, optional-->

<!--from payloads-->
  |pounds   =  <!--Payload mass in pounds, optional-->

<!--from stages-->
  |alt-thrust =  <!--thrust provided by a single booster/stage in pounds-force, optional-->
  |alt-total  =  <!--total thrust for all boosters in pounds-force, optional-->

Microformat

The HTML mark-up produced by this template includes an hProduct microformat that makes a product's details readily parsable by computer programs. This aids tasks such as the cataloguing of articles and maintenance of databases. For more information about the use of microformats on Wikipedia, please visit the Microformat WikiProject.

If the product has a URL, use {{URL}} to include it.

Classes used

The HTML classes of this microformat include:

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• category
• description
• fn
• hproduct
• identifier
• listing
• photo
• price
• review
• type
• url
• value

Please do not rename or remove these classes
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Tracking categories

• Category:Rocketry articles with outdated infoboxes (26)
• Category:Pages using infobox rocket with unknown parameters (0)