ढाँचा:Infobox rocket/कागजात

Usage

{{Infobox rocket
<!----Image (optional)---->
|image   =  <!--image filename (omit "Image:" prefix), required-->
|imsize  =  <!--Size of image (omit "px" suffix), optional, defaults to 270px-->
|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-->
|place-origin   =  <!--place of origin, optional-->
<!----Costs (optional)---->
|cpl      =  <!--cost per launch, required-->
|cpl-year =  <!--year when this cost applied, required-->
|alt-cpl  =  <!--cost in alternative currency, optional-->
<!----Dimensions (required)---->
|height       =  <!--height of the rocket in metres, required, use {{convert}}-->
|diameter     =  <!--core diameter in metres, required, use {{convert}}-->
|mass         =  <!--mass of rocket in kilograms, required, use {{convert}}-->
|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]].-->
  |kilos    =  <!--Payload mass in kilograms, required, use {{convert}}-->
  }}
<!----Associated rockets (optional)---->
|family      =  <!--rocket family, 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-->
|first    =  <!--date of maiden flight, optional-->
|last     =  <!--date of final flight, optional-->
|only     =  <!--launch date if only one was launched, optional-->
|payloads =  <!--associated 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-->
  |name       =  <!--name of the stage/booster, optional-->
  |number     =  <!--number of boosters, required if type = booster-->
  |length     =  <!--length of a single booster/stage in metres, optional, use {{convert}}-->
  |diameter   =  <!--diameter of a single booster/stage, optional in metres, use {{convert}}-->
  |empty      =  <!--empty mass of a single booster/stage in kilograms, optional, use {{convert}}-->
  |gross      =  <!--gross (fuelled) mass of a single booster/stage, optional--> 
  |engines    =  <!--number and type of engines used on each individual booster/stage, required-->
  |thrust     =  <!--thrust provided by a single booster/stage in kN, required, use {{convert}}-->
  |total      =  <!--total thrust for all boosters in kN, optional, use {{convert}}-->
  |SI         =  <!--specific impulse of an individual booster/stage, in secs, optional-->
  |burntime   =  <!--burn time, required-->
  |fuel       =  <!--fuel 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 secs, optional-->
|boostertime    =  <!--burn time, required-->
|boosterfuel    =  <!--fuel 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 secs, optional-->
|alt-boostertime     =  <!--burn time, required-->
|alt-boosterfuel     =  <!--fuel 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 secs, optional-->
|alt2-boostertime    =  <!--burn time, required-->
|alt2-boosterfuel    =  <!--fuel 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 secs, optional-->
|stage1time     =  <!--burn time, required-->
|stage1fuel     =  <!--fuel used in stage, required-->
<!--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 secs, optional-->
|stage1atime    =  <!--burn time, required-->
|stage1afuel    =  <!--fuel used in stage, required-->
<!--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 secs, optional-->
|stage2time     =  <!--burn time, required-->
|stage2fuel     =  <!--fuel 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 secs, optional-->
|stage2atime    =  <!--burn time, required-->
|stage2afuel    =  <!--fuel 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 secs, optional-->
|stage3time     =  <!--burn time, required-->
|stage3fuel     =  <!--fuel 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 secs, 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 secs, optional-->
|stage4time     =  <!--burn time, required-->
|stage4fuel     =  <!--fuel 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 secs, optional-->
|stage5time     =  <!--burn time, required-->
|stage5fuel     =  <!--fuel 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 secs, optional-->
|stage6time     =  <!--burn time, required-->
|stage6fuel     =  <!--fuel 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, which makes the product's details parsable by computers, either acting automatically to index articles across Wikipedia for search engines, or via a browser tool operated by a person. For more information about the use of microformats on Wikipedia, please see the microformat project.

If the product has a URL, use {{URL}}.

hProduct uses HTML classes including:

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

Please do not rename or remove these classes; nor collapse nested elements which use them.