Template:Infobox rocket/doc

Usage

Copyable guide

{{{name}}} [[File:{{{logo}}}|frameless|alt={{{logo_alt}}}|upright={{{logo_upright}}}]] [[File:{{{image}}}|frameless|alt={{{alt}}}|upright={{{upright}}}]] {{{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}}} Based on {{{derived_from}}} Derivative work {{{derivatives}}} Comparable {{{comparable}}} Launch history Status {{{Status}}} Launch sites {{{sites}}} Total launches {{{launches}}} Success(es) {{{success}}} Failure(s) {{{fail}}} Partial failure(s) {{{partial}}} Notable outcome(s) {{{other_outcome}}} Landings {{{landings}}} First flight {{{first}}} Last flight {{{last}}} UTC date of spacecraft launch {{{only}}} Type of passengers/cargo {{{payloads}}} Boosters ({{{diff}}}) - {{{boostername}}} {{{stagedata}}} 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}}} Destroyed before launch {{{destroyedbefore}}} {{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--> |dry mass = <!--mass of unfueled rocket in kilograms, use {{cvt|MASS|kg}}, optional--> |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 (e.g. 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--> |destroyedbefore = <!--total number of rockets destroyed before/in preparation for launch--> |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 (e.g. 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.

Tip: use |capacities={{infobox rocket/payload|location=[[low Earth orbit]]|mass={{cvt|XXXXX|kg}}}} for LEO

Copyable template

{{{name}}} [[File:{{{logo}}}|frameless|alt={{{logo_alt}}}|upright={{{logo_upright}}}]] [[File:{{{image}}}|frameless|alt={{{alt}}}|upright={{{upright}}}]] {{{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}}} Based on {{{derived_from}}} Derivative work {{{derivatives}}} Comparable {{{comparable}}} Launch history Status {{{Status}}} Launch sites {{{sites}}} Total launches {{{launches}}} Success(es) {{{success}}} Failure(s) {{{fail}}} Partial failure(s) {{{partial}}} Notable outcome(s) {{{other_outcome}}} Landings {{{landings}}} First flight {{{first}}} Last flight {{{last}}} UTC date of spacecraft launch {{{only}}} Type of passengers/cargo {{{payloads}}} Boosters ({{{diff}}}) - {{{boostername}}} {{{stagedata}}} 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}}} Destroyed before launch {{{destroyedbefore}}} <!--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-->

Wikidata

This template is using Wikidata with opt-out available. Opt-out here means that the template enables Wikidata by default, and only suppressed if the fields are manually written. It will probably stay like this for a very long time, until almost all information has been migrated.

Note: It is impossible to turn off Wikidata without manually entering values.

Why now?

A lot of people are concerned about Wikidata's information quality, and while this is a legitimate concern, it is very impractical. Most info in infoboxes are never cited, but rather being cited at the article itself or even not cited at all. Infoboxes are also extremely hard to be corrected by new editors, and Wikidata (although still pretty hard to use) is a bit more friendlier to them. The biggest concern however is that without introduction Wikidata will not be able to be populated quickly. It will not be filled with vandalism however as it will only show up for autoconfirmed users so data quality is increased drastically.

Another reason for Wikidata is synchronization. With a rise of private spaceflight and such, this is a perfect opportunity to add more data and collaborate between Wikipedias. By migrating information to Wikidata, information can be written quickly and accurately, and with the rise of Wikifunction it might not be long that having local infobox is obsolete.

Wait! What about Template:Infobox rocket stage?

Template:Infobox rocket stage uses a subtemplate of Template:Infobox rocket called Template:Infobox rocket/stage. In the first phase of Wikidata transition, these engines will still technically supported, but without Wikidata functionality. Template:Infobox rocket stage will be completely revamped in the future. This is what happens when you're being lazy and don't future-proof your work

Wikibase items

Note: Legacy infobox is not supported due to immense complexity and high risk

List of parameters corresponding to Wikibase items

|logo         = [manual input]
|logo_upright = [manual input]
|image        = [manual input]
|upright      = [manual input]
|caption      = [manual input]

|name           = [item label]
|function       = has use (P366)
|manufacturer   = manufacturer (P176) [with nested] of (P642)
|country-origin = country of origin (P495)

|pcost    = capital cost (P2130) [of nested] criterion used (P1013) [that has] whole (Q16868672)
|cpl      = capital cost (P2130) [of nested] criterion used (P1013) [that has] rocket launch (Q797476)
|alt-cpl  = [not used]
|cpl-year = capital cost (P2130) [of nested] criterion used (P1013) [that has] year (Q577)

|height       = height (P2048)
|diameter     = diameter (P2386)
|width        = width (P2049)
|mass         = mass (P2067)
|drymass      = [manual input]
|stages       = has part(s) (P527) [with nested] quantity (P1114)

|capacities    = [Uses Template:Infobox rocket/payload, need |to= having destination's QID number]
  |location    = [qid input to |to=]
  |altitude    = destination point (P1444) [nested] [|to=] [at] apoapsis (P2243), choose this property because elevation above sea level (P2044) limits to 100km and this is an often advertised value
  |inclination = destination point (P1444) [nested] [|to=] [at] orbital inclination (P2045)
  |mass        = destination point (P1444) [nested] [|to=] [at] payload mass (P4519) 
  |volume      = destination point (P1444) [nested] [|to=] [at] volume as quantity (P2234)

|family       = subclass of (P279) [of nested] criterion used (P1013) [that has] rocket family (Q109542585)
|derived_from = based on (P144)
|derivatives  = derivative work (P4969)
|comparable   = [manual input]

|status   = state of use (P5817)
|sites    = start point (P1427)
|launches = quantity (P1114) [of nested] criterion used (P1013) [that has] rocket launch (Q797476)
|success  = quantity (P1114) [of nested] has characteristic (P1552) [that has] success (Q7632586)
|fail     = quantity (P1114) [of nested] has characteristic (P1552) [that has] failure (Q1121708)
|partial  = quantity (P1114) [of nested] has characteristic (P1552) [that has] breakdown (Q28777323)
|destroyedbefore = [manual input]
|other_outcome   = significant event (P793) [of nested] has cause (P828) [that has] notability (Q4993710)
|landings = quantity (P1114) [of nested] has characteristic (P1552) [that has] landing (Q844947)
|first    = significant event (P793) [of nested] has cause (P828) [that has] first (Q19269277)
|last     = significant event (P793) [of nested] has cause (P828) [that has] last (Q30013662)
|only     = UTC date of spacecraft launch (P619)
|payloads = type of passengers/cargo (P3437)

|stagedata    = [Uses Template:Infobox rocket/stage, need |to= having stage's QID number]
  |type       = [manual input]
  |diff       = part of (P361)
  |stageno    = [manual input]*
  |name       = [item label]
  |number     = quantity (P1114) [of nested] criterion used (P1013) [that has] [vehicle's QID]
  |length     = height (P2048)
  |diameter   = diameter (P2386)
  |width      = width (P2049)
  |empty      = mass (P2067) [of nested] criterion used (P1013) [that has] dry weight (Q1140878)
  |gross      = mass (P2067) [of nested] together with (P1706) [that has] propellant (Q1364934)
  |propmass   = mass (P2067) [of nested] criterion used (P1013) [that has] propellant (Q1364934)
  |engines    = powered by (P516) [with nested] quantity (P1114)
  |solid      = [manual input]
  |thrust     = maximum thrust (P2228) [of nested] criterion used (P1013) [that has] identity (Q254474)
  |total      = maximum thrust (P2228) [of nested] criterion used (P1013) [that has] [vehicle's QID]
  |SI         = [manual input]^
  |burntime   = duration (P2047) [of nested] criterion used (P1013) [that has] combustion (Q133235)
  |fuel       = source of energy (P618)
  
^: Property that is going to be added
*: Implement once lexeme is allowed in wikipedia

List of labels using Wikidata properties

Information at Wikidata will display in this infobox only if a reference to a reliable source is provided for that wikidata item, per this 2018 RFC.

|logo         = [manual input]
|logo_upright = [manual input]
|image        = [manual input]
|upright      = [manual input]
|caption      = [manual input]

|name           = [item label]
|function       = has use (P366)
|manufacturer   = manufacturer (P176)
|country-origin = country of origin (P495)

|pcost    = [manual input]
|cpl      = [manual input]
|alt-cpl  = [not used]
|cpl-year = [manual input]

|height       = height (P2048)
|diameter     = diameter (P2386)
|width        = width (P2049)
|mass         = mass (P2067)
|dry mass     = [manual input]
|stages       = [manual input]

|capacities    = [Uses Template:Infobox rocket/payload, need |to= having destination's QID number]
  |location    = [manual input]
  |altitude    = [manual input]
  |inclination = orbital inclination (P2045)
  |mass        = mass (P2067)
  |volume      = [manual input]

|family       = [manual input]
|derived_from = based on (P144)
|derivatives  = derivative work (P4969)
|comparable   = [manual input]

|status   = [manual input]
|sites    = [manual input]
|launches = [manual input]
|success  = [manual input]
|fail     = [manual input]
|partial  = [manual input]
|destroyedbefore = [manual input]
|other_outcome   = [manual input]
|landings = [manual input]
|first    = [manual input]
|last     = [manual input]
|only     = UTC date of spacecraft launch (P619)
|payloads = type of passengers/cargo (P3437)

|stagedata    = [Uses Template:Infobox rocket/stage, need |to= having stage's QID number]
  |type       = [manual input]
  |diff       = [manual input]
  |stageno    = [manual input]
  |name       = [item label]
  |number     = [manual input]
  |length     = height (P2048)
  |diameter   = diameter (P2386)
  |width      = width (P2049)
  |empty      = [manual input]
  |gross      = [manual input]
  |propmass   = [manual input]
  |engines    = powered by (P516)
  |solid      = [manual input]
  |thrust     = maximum thrust (P2228)
  |total      = [manual input]
  |SI         = [manual input]
  |burntime   = [manual input]
  |fuel       = [manual input]

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:

• 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.

Tracking categories

• Category:Rocketry articles with outdated infoboxes (64)
• Category:Pages using infobox rocket with unknown parameters (1)