سانچہ:خانہ معلومات راکٹ

دستاویز [نمائش] [ترمیم] [تاریخچہ] [تطہیر]

This documentation is transcluded from سانچہ:Infobox rocket/doc (ترمیم | تبادلۂ خیال | تاریخچہ | روابط | زیر نظر | نوشتہ جات). 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}}}|{{{logo_alt}}}]] [[File:{{{image}}}|frameless|alt={{{alt}}}|upright={{{upright}}}|{{{alt}}}]] {{{caption}}} کام {{{function}}} راکٹ ساز {{{manufacturer}}} اصل ملک {{{country-origin}}} لاگت منصوبہ {{{pcost}}} لاگت فی نانچ {{{cpl}}} ({{{alt-cpl}}}) لاگت فی سال {{{cpl-year}}} حجم بلندی {{{height}}} ({{{alt-height}}}) رداس {{{diameter}}} ({{{alt-diameter}}}) چوڑائی {{{width}}} ({{{alt-width}}}) حجم {{{mass}}} ({{{alt-mass}}}) اسٹیج {{{stages}}} اہلیت {{{capacities}}} پےلوڈ تا زیریں زمینی مدار {{{LEO-payload}}} ({{{alt-LEO}}}) پےلوڈ تا {{{payload-location}}} {{{payload}}} ({{{alt-payload}}}) پےلوڈ تا {{{payload2-location}}} {{{payload2}}} ({{{alt-payload2}}}) پےلوڈ تا {{{payload3-location}}} {{{payload3}}} ({{{alt-payload3}}}) پےلوڈ تا {{{payload4-location}}} {{{payload4}}} ({{{alt-payload4}}}) پےلوڈ تا {{{payload5-location}}} {{{payload5}}} ({{{alt-payload5}}}) Associated rockets خاندان {{{family}}} Derivatives {{{derivatives}}} Comparable {{{comparable}}} تاریخ لانچ کیفیت {{{status}}} مقامات نانچ {{{sites}}} کل لانچ {{{launches}}} کامیاب {{{success}}} ناکام {{{fail}}} جزوی ناکام {{{partial}}} دیگر {{{other_outcome}}} لینڈنگ {{{landings}}} پہلی پرواز {{{first}}} آخری پرواز {{{last}}} تاریخ لانچ {{{only}}} قابل ذکر پےلوڈ {{{payloads}}} {{{stagedata}}}Boosters ({{{diff}}}) - {{{boostername}}} No. boosters {{{boosters}}} انجن {{{boosterengines}}} قوت دھکیل {{{boosterthrust}}} ({{{alt-boosterthrust}}}) کل قوت دھکیل {{{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}}} انجن {{{stage4engines}}} قوت دھکیل {{{stage4thrust}}} ({{{alt-stage4thrust}}}) Specific impulse {{{stage4SI}}} Burn time {{{stage4time}}} Propellant {{{stage4fuel}}} Fifth stage - {{{stage5name}}} انجن {{{stage5engines}}} قوت دھکیل {{{stage5thrust}}} ({{{alt-stage5thrust}}}) Specific impulse {{{stage5SI}}} Burn time {{{stage5time}}} Propellant {{{stage5fuel}}} Sixth stage - {{{stage6name}}} انجن {{{stage6engines}}} قوت دھکیل {{{stage6thrust}}} ({{{alt-stage6thrust}}}) Specific impulse {{{stage6SI}}} Burn time {{{stage6time}}} Propellant {{{stage6fuel}}} {{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 [[زیریں زمینی مدار]] 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 {{تحویل|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=[[زیریں زمینی مدار]]|mass={{cvt|XXXXX|kg}}}} for LEO Copyable template {{{name}}} [[File:{{{logo}}}|frameless|alt={{{logo_alt}}}|upright={{{logo_upright}}}|{{{logo_alt}}}]] [[File:{{{image}}}|frameless|alt={{{alt}}}|upright={{{upright}}}|{{{alt}}}]] {{{caption}}} کام {{{function}}} راکٹ ساز {{{manufacturer}}} اصل ملک {{{country-origin}}} لاگت منصوبہ {{{pcost}}} لاگت فی نانچ {{{cpl}}} ({{{alt-cpl}}}) لاگت فی سال {{{cpl-year}}} حجم بلندی {{{height}}} ({{{alt-height}}}) رداس {{{diameter}}} ({{{alt-diameter}}}) چوڑائی {{{width}}} ({{{alt-width}}}) حجم {{{mass}}} ({{{alt-mass}}}) اسٹیج {{{stages}}} اہلیت {{{capacities}}} پےلوڈ تا زیریں زمینی مدار {{{LEO-payload}}} ({{{alt-LEO}}}) پےلوڈ تا {{{payload-location}}} {{{payload}}} ({{{alt-payload}}}) پےلوڈ تا {{{payload2-location}}} {{{payload2}}} ({{{alt-payload2}}}) پےلوڈ تا {{{payload3-location}}} {{{payload3}}} ({{{alt-payload3}}}) پےلوڈ تا {{{payload4-location}}} {{{payload4}}} ({{{alt-payload4}}}) پےلوڈ تا {{{payload5-location}}} {{{payload5}}} ({{{alt-payload5}}}) Associated rockets خاندان {{{family}}} Derivatives {{{derivatives}}} Comparable {{{comparable}}} تاریخ لانچ کیفیت {{{status}}} مقامات نانچ {{{sites}}} کل لانچ {{{launches}}} کامیاب {{{success}}} ناکام {{{fail}}} جزوی ناکام {{{partial}}} دیگر {{{other_outcome}}} لینڈنگ {{{landings}}} پہلی پرواز {{{first}}} آخری پرواز {{{last}}} تاریخ لانچ {{{only}}} قابل ذکر پےلوڈ {{{payloads}}} {{{stagedata}}}Boosters ({{{diff}}}) - {{{boostername}}} No. boosters {{{boosters}}} انجن {{{boosterengines}}} قوت دھکیل {{{boosterthrust}}} ({{{alt-boosterthrust}}}) کل قوت دھکیل {{{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}}} انجن {{{stage4engines}}} قوت دھکیل {{{stage4thrust}}} ({{{alt-stage4thrust}}}) Specific impulse {{{stage4SI}}} Burn time {{{stage4time}}} Propellant {{{stage4fuel}}} Fifth stage - {{{stage5name}}} انجن {{{stage5engines}}} قوت دھکیل {{{stage5thrust}}} ({{{alt-stage5thrust}}}) Specific impulse {{{stage5SI}}} Burn time {{{stage5time}}} Propellant {{{stage5fuel}}} Sixth stage - {{{stage6name}}} انجن {{{stage6engines}}} قوت دھکیل {{{stage6thrust}}} ({{{alt-stage6thrust}}}) Specific impulse {{{stage6SI}}} Burn time {{{stage6time}}} Propellant {{{stage6fuel}}} <!--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 = استعمال (P366) manufacturer = صانع (P176) [with nested] (P642) country-origin = اصل ملک (P495) pcost = لاگت (P2130) [of nested] مستعمل معیار (P1013) [that has] whole (Q16868672) cpl = لاگت (P2130) [of nested] مستعمل معیار (P1013) [that has] rocket launch (Q797476) alt-cpl = [not used] cpl-year = لاگت (P2130) [of nested] مستعمل معیار (P1013) [that has] سال (Q577) height = قد (P2048) diameter = قطر (P2386) width = اونچائی (P2049) mass = وزن (P2067) drymass = [manual input] stages = جزو (P527) [with nested] تعداد (P1114) capacities = [Uses Template:Infobox rocket/payload, need |to= having destination's QID number] to=] altitude = destination point (P1444) [nested] [|to=] [at] apoapsis (P2243), choose this property because سطح سمندر سے بلندی (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 = خاصیت کا اعلیٰ درجہ (P279) [of nested] مستعمل معیار (P1013) [that has] rocket family (Q109542585) derived_from = ماخوذ از (P144) derivatives = مشتق کام (P4969) comparable = [manual input] status = state of use (P5817) sites = start point (P1427) launches = تعداد (P1114) [of nested] مستعمل معیار (P1013) [that has] rocket launch (Q797476) success = تعداد (P1114) [of nested] خیال (P1552) [that has] کامیابی (Q7632586) fail = تعداد (P1114) [of nested] خیال (P1552) [that has] ناکامی (Q1121708) partial = تعداد (P1114) [of nested] خیال (P1552) [that has] breakdown (Q28777323) destroyedbefore = [manual input] other_outcome = قابل ذکر (P793) [of nested] وجہ (P828) [that has] notability (Q4993710) landings = تعداد (P1114) [of nested] خیال (P1552) [that has] اتار (Q844947) first = قابل ذکر (P793) [of nested] وجہ (P828) [that has] first (Q19269277) last = قابل ذکر (P793) [of nested] وجہ (P828) [that has] آخری (Q30013662) only = UTC date of spacecraft launch (P619) payloads = carries passengers or cargo (P3437) stagedata = [Uses Template:Infobox rocket/stage, need |to= having stage's QID number] type = [manual input] diff = کا حصہ (P361) stageno = [manual input]* name = [item label] number = تعداد (P1114) [of nested] مستعمل معیار (P1013) [that has] [vehicle's QID] length = قد (P2048) diameter = قطر (P2386) width = اونچائی (P2049) empty = وزن (P2067) [of nested] مستعمل معیار (P1013) [that has] dry weight (Q1140878) gross = وزن (P2067) [of nested] بالاشتراک مع (P1706) [that has] پروپیلنٹ (Q1364934) propmass = وزن (P2067) [of nested] مستعمل معیار (P1013) [that has] پروپیلنٹ (Q1364934) engines = انجن (P516) [with nested] تعداد (P1114) solid = [manual input] thrust = maximum thrust (P2228) [of nested] مستعمل معیار (P1013) [that has] identity (Q254474) total = maximum thrust (P2228) [of nested] مستعمل معیار (P1013) [that has] [vehicle's QID] SI = [manual input]^ burntime = دورانیہ (P2047) [of nested] مستعمل معیار (P1013) [that has] احتراق (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 = استعمال (P366) manufacturer = صانع (P176) country-origin = اصل ملک (P495) pcost = [manual input] cpl = [manual input] alt-cpl = [not used] cpl-year = [manual input] height = قد (P2048) diameter = قطر (P2386) width = اونچائی (P2049) mass = وزن (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 = وزن (P2067) volume = [manual input] family = [manual input] derived_from = ماخوذ از (P144) derivatives = مشتق کام (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 = carries passengers or 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 = قد (P2048) diameter = قطر (P2386) width = اونچائی (P2049) empty = [manual input] gross = [manual input] propmass = [manual input] engines = انجن (P516) solid = [manual input] thrust = maximum thrust (P2228) total = [manual input] SI = [manual input] burntime = [manual input] fuel = [manual input] Microformat Tracking categories زمرہ:Rocketry articles with outdated infoboxes (5) زمرہ:Pages using infobox rocket with unknown parameters (2)