Template:Infobox rocket/doc

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Usage
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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 =
 * alt-LEO    =


 * payload-location =
 * payload          =
 * alt-payload      =


 * payload2-location =
 * payload2         =
 * alt-payload2     =


 * payload3-location =
 * payload3         =
 * alt-payload3     =


 * payload4-location =
 * payload4         =
 * alt-payload4     =


 * payload5-location =
 * payload5         =
 * alt-payload5     =


 * diff          =
 * boostername   =
 * boosters      =  <--number of booster rockets present, required-->
 * boosterengines =
 * boosterthrust =
 * alt-boosterthurst =
 * boosterTT     =
 * alt-boosterTT =
 * boosterSI     =
 * boostertime   =
 * boosterfuel   =


 * alt-diff           =
 * alt-boostername    =
 * alt-boosters       =  <--number of booster rockets present, required-->
 * alt-boosterengines =
 * alt-boosterthrust  =  <!-thrust provided by a single booster in kN, required-->
 * alt-alt-boosterthurst =
 * alt-boosterSI      =
 * alt-boostertime    =
 * alt-boosterfuel    =


 * alt2-diff          =
 * alt2-boostername   =
 * alt2-boosters      =  <--number of booster rockets present, required-->
 * alt2-boosterengines =
 * alt2-boosterthrust =  <!-thrust provided by a single booster in kN, required-->
 * alt2-alt-boosterthurst =
 * alt2-boosterSI     =
 * alt2-boostertime   =
 * alt2-boosterfuel   =


 * stage1diff    =
 * stage1name    =
 * stage1engines =
 * stage1thrust  =  <!-thrust provided by stage in kN, required-->
 * alt-stage1thurst =
 * stage1SI      =
 * stage1time    =
 * stage1fuel    =
 * stage1fueloxidizermassvolume =


 * stage1adiff   =
 * stage1aname   =
 * stage1aengines =
 * stage1athrust =  <!-thrust provided by stage in kN, required-->
 * alt-stage1athurst =
 * stage1aSI     =
 * stage1atime   =
 * stage1afuel   =
 * stage1afueloxidizermassvolume =


 * stage2diff    =
 * stage2name    =
 * stage2engines =
 * stage2thrust  =  <!-thrust provided by stage in kN, required-->
 * alt-stage2thurst =
 * stage2SI      =
 * stage2time    =
 * stage2fuel    =


 * stage2adiff   =
 * stage2aname   =
 * stage2aengines =
 * stage2athrust =  <!-thrust provided by stage in kN, required-->
 * alt-stage2athurst =
 * stage2aSI     =
 * stage2atime   =
 * stage2afuel   =


 * stage3diff    =
 * stage3name    =
 * stage3engines =
 * stage3thrust  =  <!-thrust provided by stage in kN, required-->
 * alt-stage3thurst =
 * stage3SI      =
 * stage3time    =
 * stage3fuel    =


 * stage3adiff   =
 * stage3aname   =
 * stage3aengines =
 * stage3athrust =  <!-thrust provided by stage in kN, required-->
 * alt-stage3athurst =
 * stage3aSI     =
 * stage3atime   =
 * stage3afuel   =


 * stage4diff    =
 * stage4name    =
 * stage4engines =
 * stage4thrust  =  <!-thrust provided by stage in kN, required-->
 * alt-stage4thurst =
 * stage4SI      =
 * stage4time    =
 * stage4fuel    =


 * stage5diff    =
 * stage5name    =
 * stage5engines =
 * stage5thrust  =  <!-thrust provided by stage in kN, required-->
 * alt-stage5thurst =
 * stage5SI      =
 * stage5time    =
 * stage5fuel    =


 * stage6diff    =
 * stage6name    =
 * stage6engines =
 * stage6thrust  =  <!-thrust provided by stage in kN, required-->
 * alt-stage6thurst =
 * stage6SI      =
 * stage6time    =
 * stage6fuel    =


 * alt-height  =
 * alt-diameter =
 * alt-mass    =

|pounds  =

|alt-thrust = |alt-total =

Microformat
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