টেমপ্লেট:তথ্যছক রকেট

টেমপ্লেট:তথ্যছক রকেট
উইকিমিডিয়া টেমপ্লেট
[উইকিউপাত্তে সম্পাদনা করুন]

টেমপ্লেট নথি[দেখুন] [সম্পাদনা] [ইতিহাস] [শোধন]

This documentation is transcluded from টেমপ্লেট:Infobox rocket/doc (সম্পাদনা | আলোচনা | ইতিহাস | সংযোগ | নজর | লগ). The edit link for this section can be used to edit the original documentation.

Usage

Copyable guide

{{{name}}} উইকিমিডিয়া টেমপ্লেট [[File:{{{logo}}}|frameless|alt={{{logo_alt}}}|upright={{{logo_upright}}}|{{{logo_alt}}}]] [[File:{{{image}}}|frameless|alt={{{alt}}}|upright={{{upright}}}|{{{alt}}}]] {{{caption}}} ব্যবহার {{{function}}} প্রস্তুতকারক {{{manufacturer}}} উৎপত্তির দেশ {{{country-origin}}} প্রকল্প ব্যয় {{{pcost}}} উৎক্ষেপণ প্রতি ব্যয় {{{cpl}}} ({{{alt-cpl}}}) বছর প্রতি ব্যয় {{{cpl-year}}} আকার উচ্চতা {{{height}}} ({{{alt-height}}}) ব্যাস {{{diameter}}} ({{{alt-diameter}}}) প্রস্থ {{{width}}} ({{{alt-width}}}) ভর {{{mass}}} ({{{alt-mass}}}) পর্যায় {{{stages}}} {{{capacities}}} সহযোগী রকেট পরিবার {{{family}}} এর উপর ভিত্তি করে {{{derived_from}}} ব্যুৎপন্ন কর্ম {{{derivatives}}} উৎক্ষেপণ ইতিহাস অবস্থা {{{Status}}} উৎক্ষেপণ স্থান {{{sites}}} মোট উৎক্ষেপণ {{{launches}}} সফল {{{success}}} ব্যর্থ {{{fail}}} আংশিক ব্যর্থ {{{partial}}} উল্লেখযোগ্য ফল {{{other_outcome}}} অবতরণ {{{landings}}} প্রথম উড়ান {{{first}}} শেষ উড়ান {{{last}}} মহাকাশযান ওড়ার সময় {{{only}}} মানুষ বা পণ্য পরিবহন {{{payloads}}} {{{stagedata}}} উৎক্ষেপণের আগে ধ্বংস {{{destroyedbefore}}} [উইকিউপাত্তে সম্পাদনা করুন] {{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--> |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}}} উইকিমিডিয়া টেমপ্লেট [[File:{{{logo}}}|frameless|alt={{{logo_alt}}}|upright={{{logo_upright}}}|{{{logo_alt}}}]] [[File:{{{image}}}|frameless|alt={{{alt}}}|upright={{{upright}}}|{{{alt}}}]] {{{caption}}} ব্যবহার {{{function}}} প্রস্তুতকারক {{{manufacturer}}} উৎপত্তির দেশ {{{country-origin}}} প্রকল্প ব্যয় {{{pcost}}} উৎক্ষেপণ প্রতি ব্যয় {{{cpl}}} ({{{alt-cpl}}}) বছর প্রতি ব্যয় {{{cpl-year}}} আকার উচ্চতা {{{height}}} ({{{alt-height}}}) ব্যাস {{{diameter}}} ({{{alt-diameter}}}) প্রস্থ {{{width}}} ({{{alt-width}}}) ভর {{{mass}}} ({{{alt-mass}}}) পর্যায় {{{stages}}} {{{capacities}}} সহযোগী রকেট পরিবার {{{family}}} এর উপর ভিত্তি করে {{{derived_from}}} ব্যুৎপন্ন কর্ম {{{derivatives}}} উৎক্ষেপণ ইতিহাস অবস্থা {{{Status}}} উৎক্ষেপণ স্থান {{{sites}}} মোট উৎক্ষেপণ {{{launches}}} সফল {{{success}}} ব্যর্থ {{{fail}}} আংশিক ব্যর্থ {{{partial}}} উল্লেখযোগ্য ফল {{{other_outcome}}} অবতরণ {{{landings}}} প্রথম উড়ান {{{first}}} শেষ উড়ান {{{last}}} মহাকাশযান ওড়ার সময় {{{only}}} মানুষ বা পণ্য পরিবহন {{{payloads}}} {{{stagedata}}} উৎক্ষেপণের আগে ধ্বংস {{{destroyedbefore}}} [উইকিউপাত্তে সম্পাদনা করুন] <!--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 avaliable. Opt-out here means that the template enable Wikidata by default, and only being suppressed if the fields are manually written. It would probably stay like this for a very long time, until almost all information has being 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. Infobox is 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 never be able to be populated quickly. It will not be filled with vandalism however, it would 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 transistion, these engines will still technically supported, but without Wikidata functionality. Template:Infobox rocket stage will be completely rewamped 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 corrosponding to Wikibase items

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

|name           = [item label]
|function       = ব্যবহার (P366)
|manufacturer   = প্রস্তুতকারক (P176) [with nested] এর (P642)
|country-origin = উৎপত্তির দেশ (P495)

|pcost    = খরচ (P2130) [of nested] ব্যবহৃত মানদণ্ড (P1013) [that has] whole (Q16868672)
|cpl      = খরচ (P2130) [of nested] ব্যবহৃত মানদণ্ড (P1013) [that has] রকেট উত্থাপন (Q797476)
|alt-cpl  = [not used]
|cpl-year = খরচ (P2130) [of nested] ব্যবহৃত মানদণ্ড (P1013) [that has] বছর (Q577)

|height       = উচ্চতা (P2048)
|diameter     = ব্যাস (P2386)
|width        = প্রস্থ (P2049)
|mass         = ভর (P2067)
|stages       = এর অংশ (P527) [with nested] পরিমাণ (P1114)

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

|family       = যার উপশ্রেণী (P279) [of nested] ব্যবহৃত মানদণ্ড (P1013) [that has] rocket family (Q109542585)
|derived_from = এর উপর ভিত্তি করে (P144)
|derivatives  = ব্যুৎপন্ন কর্ম (P4969)
|comparable   = [manual input]

|status   = অবস্থা (P5817)
|sites    = যাত্রা শুরুর স্থান (P1427)
|launches = পরিমাণ (P1114) [of nested] ব্যবহৃত মানদণ্ড (P1013) [that has] রকেট উত্থাপন (Q797476)
|success  = পরিমাণ (P1114) [of nested] যে গুণমান আছে (P1552) [that has] সফলতা (Q7632586)
|fail     = পরিমাণ (P1114) [of nested] যে গুণমান আছে (P1552) [that has] ব্যর্থতা (Q1121708)
|partial  = পরিমাণ (P1114) [of nested] যে গুণমান আছে (P1552) [that has] breakdown (Q28777323)
|destroyedbefore = [manual input]
|other_outcome   = উল্লেখযোগ্য ঘটনা (P793) [of nested] যার কারণ (P828) [that has] notability (Q4993710)
|landings = পরিমাণ (P1114) [of nested] যে গুণমান আছে (P1552) [that has] অবতরণ (Q844947)
|first    = উল্লেখযোগ্য ঘটনা (P793) [of nested] যার কারণ (P828) [that has] first (Q19269277)
|last     = উল্লেখযোগ্য ঘটনা (P793) [of nested] যার কারণ (P828) [that has] last (Q30013662)
|only     = মহাকাশযান ওড়ার সময় (P619)
|payloads = মানুষ বা পণ্য পরিবহন (P3437)

|stagedata    = [Uses Template:Infobox rocket/stage, need |to= having stage's QID number]
  |type       = [manual input]
  |diff       = যার অংশ (P361)
  |stageno    = [manual input]*
  |name       = [item label]
  |number     = পরিমাণ (P1114) [of nested] ব্যবহৃত মানদণ্ড (P1013) [that has] [vehicle's QID]
  |length     = উচ্চতা (P2048)
  |diameter   = ব্যাস (P2386)
  |width      = প্রস্থ (P2049)
  |empty      = ভর (P2067) [of nested] ব্যবহৃত মানদণ্ড (P1013) [that has] পরিচয় (Q254474)
  |gross      = ভর (P2067) [of nested] এর সাথে (P1706) [that has] propellant (Q1364934)
  |propmass   = ভর (P2067) [of nested] ব্যবহৃত মানদণ্ড (P1013) [that has] propellant (Q1364934)
  |engines    = যা দ্বারা চালিত (P516) [with nested] পরিমাণ (P1114)
  |solid      = [manual input]
  |thrust     = সর্বোচ্চ ঘাত (P2228) [of nested] ব্যবহৃত মানদণ্ড (P1013) [that has] পরিচয় (Q254474)
  |total      = সর্বোচ্চ ঘাত (P2228) [of nested] ব্যবহৃত মানদণ্ড (P1013) [that has] [vehicle's QID]
  |SI         = [manual input]^
  |burntime   = স্থিতিকাল (P2047) [of nested] ব্যবহৃত মানদণ্ড (P1013) [that has] দহন (Q133235)
  |fuel       = শক্তির উৎস (P618)
  
^: Property that is going to be added
*: Implement once lexeme is allowed in wikipedia

List of labels using Wikidata properties

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

|name           = [item label]
|function       = ব্যবহার (P366)
|manufacturer   = প্রস্তুতকারক (P176)
|country-origin = উৎপত্তির দেশ (P495)

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

|height       = উচ্চতা (P2048)
|diameter     = ব্যাস (P2386)
|width        = প্রস্থ (P2049)
|mass         = ভর (P2067)
|stages       = [manual input]

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

|family       = [manual input]
|derived_from = এর উপর ভিত্তি করে (P144)
|derivatives  = ব্যুৎপন্ন কর্ম (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     = মহাকাশযান ওড়ার সময় (P619)
|payloads = মানুষ বা পণ্য পরিবহন (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     = উচ্চতা (P2048)
  |diameter   = ব্যাস (P2386)
  |width      = প্রস্থ (P2049)
  |empty      = [manual input]
  |gross      = [manual input]
  |propmass   = [manual input]
  |engines    = যা দ্বারা চালিত (P516)
  |solid      = [manual input]
  |thrust     = সর্বোচ্চ ঘাত (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, which makes the product's details parsable by computers, either acting automatically to index articles across Wikipedia for search engines, or via a browser tool operated by a person. For more information about the use of microformats on Wikipedia, please see the microformat project.

If the product has a URL, use {{URL}}.

hProduct uses HTML classes including:

• 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

• বিষয়শ্রেণী:Rocketry articles with outdated infoboxes (৩)
• বিষয়শ্রেণী:Pages using infobox rocket with unknown parameters (০)

See also

ব্যবহার

আরও দেখুন

উপরোক্ত নথিটি টেমপ্লেট:তথ্যছক রকেট/নথি থেকে প্রতিলিপ্ত। (সম্পাদনা | ইতিহাস)
ব্যবহারকারীগণ খেলাঘর (তৈরি করুন | আয়না) এবং পরীক্ষা পাতায় (তৈরি করুন) এই টেমপ্লেট সংক্রান্ত পরীক্ষা-নিরীক্ষা করতে পারেন।
দয়া করে /নথি উপপাতায় বিষয়শ্রেণী যোগ করুন। এই টেমপ্লেটের উপপাতাসমূহ।