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Dòng 10:
{{Infobox rocket
<!----
|logo = <!--
|logo_size = <!--
|image = <!--
|image_size = <!--
|caption = <!--caption,
<!----
|name = <!--
|function = <!--
|manufacturer = <!--
|country-origin = <!--
<!----
|pcost = <!--
|cpl = <!--
|alt-cpl = <!--
|cpl-year = <!--
<!----
|height = <!--
|diameter = <!--
|width = <!--
|mass = <!--
|stages = <!--
<!----
|capacities = <!--insert one of the following templates for each payload:-->
{{Infobox rocket/payload
|location = <!--Target orbit/trajectory,
|kilos = <!--Payload mass in kilograms, use {{cvt|PAYLOAD|kg}},
}}
<!----
|family = <!--
|derivatives = <!--
|comparable = <!--
<!----Launch history (
|status = <!--current status (eg. Active, Retired, etc),
|sites = <!--launch centres and pads,
|launches = <!--total launches to date,
|success = <!--total successful launches,
|fail = <!--total failed launches,
|partial = <!--total number of launches resulting in partial failure (e.g. incorrect orbit but still usable),
|other_outcome = <!--number of launches with unknown outcomes (or in progress),
|landings = <!--total number of landings,
|first = <!--date of first flight,
|last = <!--date of latest or final flight,
|only = <!--launch date if only one was launched,
|payloads = <!--notable payloads,
<!--Stages/boosters (
|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,
|stageno = <!--position of stage in rocket, spelled out (eg. First, Second, etc),
|name = <!--name of the stage/booster,
|number = <!--number of boosters,
|length = <!--length of a single booster/stage in metres, use {{cvt|LENGTH|m}},
|diameter = <!--diameter of a single booster/stage in metres, use {{cvt|DIAMETER|m}},
|width = <!--width of a single booster/stage if not axisymmetric, use {{cvt|WIDTH|m}},
|empty = <!--empty mass of a single booster/stage in kilograms, use {{cvt|EMPTYMASS|kg}},
|gross = <!--gross (fuelled) mass of a single booster/stage, use {{cvt|GROSSMASS|kg}},
|propmass = <!--propellant mass carried by a single booster/stage in kilograms, use {{cvt|PROPMASS|kg}},
|engines = <!--number and type of engines used on each individual booster/stage,
|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}},
|total = <!--total thrust for all boosters in kN, use {{cvt|THRUST|kN}},
|SI = <!--specific impulse of an individual booster/stage, in seconds, use {{convert|ISP_IN_SECONDS|isp}},
|burntime = <!--burn time,
|fuel = <!--fuel used in stage/boosters,
}}
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