Template:Infobox rocket

Function
Project cost
Cost per launch
Cost per year
Size
Stages
Associated rockets
Family
Launch history
Status
Launch sites
Total launches
Success(es)
Failure(s)
Partial failure(s)
Notable outcome(s)
Landings
First flight
Last flight

File:Test Template Info-Icon - Version (2).svg Template documentation[view] [edit] [history] [purge]

This documentation is transcluded from Template:Infobox rocket/doc (edit | talk | history | links | watch | logs). The edit link for this section can be used to edit the original documentation.

Usage

Copyable guide

{{{name}}} [[File:{{{logo}}}|frameless|alt={{{logo_alt}}}|upright={{{logo_upright}}}]] [[File:{{{image}}}|frameless|alt={{{alt}}}|upright={{{upright}}}]] {{{caption}}} Function Project cost Cost per launch Cost per year Size 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 Comparable {{{comparable}}} Launch history Status Launch sites Total launches Success(es) Failure(s) Partial failure(s) Notable outcome(s) Landings First flight Last flight 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}}} <syntaxhighlight lang="wikitext" style="overflow:auto;"> Function Project cost Cost per launch Cost per year Size Stages Capacity Template:Infobox rocket/payload Associated rockets Family Launch history Status Launch sites Total launches Success(es) Failure(s) Partial failure(s) Notable outcome(s) Landings First flight Last flight Template:Infobox rocket/stage </syntaxhighlight>

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 Project cost Cost per launch Cost per year Size 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 Comparable {{{comparable}}} Launch history Status Launch sites Total launches Success(es) Failure(s) Partial failure(s) Notable outcome(s) Landings First flight Last flight 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}}} <syntaxhighlight lang="wikitext" style="overflow:auto;">	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 = </syntaxhighlight>

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       =  (P366)
|manufacturer   =  (P176) [with nested]  (P642)
|country-origin =  (P495)

|pcost    =  (P2130) [of nested]  (P1013) [that has]  (Q16868672)
|cpl      =  (P2130) [of nested]  (P1013) [that has]  (Q797476)
|alt-cpl  = [not used]
|cpl-year =  (P2130) [of nested]  (P1013) [that has]  (Q577)

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

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

|family       =  (P279) [of nested]  (P1013) [that has]  (Q109542585)
|derived_from =  (P144)
|derivatives  =  (P4969)
|comparable   = [manual input]

|status   =  (P5817)
|sites    =  (P1427)
|launches =  (P1114) [of nested]  (P1013) [that has]  (Q797476)
|success  =  (P1114) [of nested]  (P1552) [that has]  (Q7632586)
|fail     =  (P1114) [of nested]  (P1552) [that has]  (Q1121708)
|partial  =  (P1114) [of nested]  (P1552) [that has]  (Q28777323)
|destroyedbefore = [manual input]
|other_outcome   =  (P793) [of nested]  (P828) [that has]  (Q4993710)
|landings =  (P1114) [of nested]  (P1552) [that has]  (Q844947)
|first    =  (P793) [of nested]  (P828) [that has]  (Q19269277)
|last     =  (P793) [of nested]  (P828) [that has]  (Q30013662)
|only     =  (P619)
|payloads =  (P3437)

|stagedata    = [Uses Template:Infobox rocket/stage, need |to= having stage's QID number]
  |type       = [manual input]
  |diff       =  (P361)
  |stageno    = [manual input]*
  |name       = [item label]
  |number     =  (P1114) [of nested]  (P1013) [that has] [vehicle's QID]
  |length     =  (P2048)
  |diameter   =  (P2386)
  |width      =  (P2049)
  |empty      =  (P2067) [of nested]  (P1013) [that has]  (Q1140878)
  |gross      =  (P2067) [of nested]  (P1706) [that has]  (Q1364934)
  |propmass   =  (P2067) [of nested]  (P1013) [that has]  (Q1364934)
  |engines    =  (P516) [with nested]  (P1114)
  |solid      = [manual input]
  |thrust     =  (P2228) [of nested]  (P1013) [that has]  (Q254474)
  |total      =  (P2228) [of nested]  (P1013) [that has] [vehicle's QID]
  |SI         = [manual input]^
  |burntime   =  (P2047) [of nested]  (P1013) [that has]  (Q133235)
  |fuel       =  (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       =  (P366)
|manufacturer   =  (P176)
|country-origin =  (P495)

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

|height       =  (P2048)
|diameter     =  (P2386)
|width        =  (P2049)
|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 =  (P2045)
  |mass        =  (P2067)
  |volume      = [manual input]

|family       = [manual input]
|derived_from =  (P144)
|derivatives  =  (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     =  (P619)
|payloads =  (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     =  (P2048)
  |diameter   =  (P2386)
  |width      =  (P2049)
  |empty      = [manual input]
  |gross      = [manual input]
  |propmass   = [manual input]
  |engines    =  (P516)
  |solid      = [manual input]
  |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 (0)
• Category:Pages using infobox rocket with unknown parameters (0)

See also

The above documentation is transcluded from Template:Infobox rocket/doc. (edit | history)
Editors can experiment in this template's sandbox (create | mirror) and testcases (create) pages.
Add categories to the /doc subpage. Subpages of this template.