>RickyCourtney: Add params

2024-07-12T03:49:37Z

Add params

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{{Infobox
| title = <includeonly>{{{name|{{PAGENAMEBASE}}}}}</includeonly>
| headerstyle = background-color:#FFDEAD
| image = {{#invoke:InfoboxImage|InfoboxImage|image={{{image|}}}|size={{{image_size|{{{imsize|}}}}}}|sizedefault=frameless|upright=1.13|alt={{{alt|{{{image_alt|}}}}}}}}
| caption = {{{caption|}}}

| label1 = Country of origin
| data1 = {{{country_of_origin|}}}

| label2 = Date
| data2 = {{{date|}}}

| label3 = First flight
| data3 = {{{first_date|}}}

| label4 = Last flight
| data4 = {{{last_date|}}}

| label5 = Designer
| data5 = {{{designer|}}}

| label10 = Manufacturer
| data10 = {{{manufacturer|}}}

| label11 = Application
| data11 = {{{purpose|}}}

| label12 = Associated {{abbr|LV|launch vehicle}}
| data12 = {{{associated|}}}

| label13 = Predecessor
| data13 = {{{predecessor|}}}

| label14 = Successor
| data14 = {{{successor|}}}

| label15 = Status
| data15 = {{{status|}}}

| header20 = {{#switch: {{lc:{{{type|}}}}}
| solid = [[Solid-fuel rocket|Solid-fuel motor]]
| liquid = [[Liquid-propellant rocket|Liquid-fuel engine]]
| hybrid = [[Hybrid rocket|Hybrid engine]]
| mono|monopropellant = {{{fuel|}}} [[monopropellant]]
| #default = {{{type|}}}
}}


| label21 = Propellant
| data21 = {{#switch: {{lc:{{{type|}}}}}
| solid
| liquid
| hybrid = {{#if: {{{oxidizer|}}}{{{oxidiser|}}} | {{{oxidizer|{{{oxidiser|}}}}}} / }} {{{fuel|}}}
}}



| label22 = Grain
| data22 = {{#ifeq:{{{type|}}}|solid| {{{grain|}}} }}

| label23 = Core
| data23 = {{#ifeq:{{{type|}}}|solid| {{{core|}}} }}

| label24 = Casing
| data24 = {{#ifeq:{{{type|}}}|solid| {{{casing|}}} }}

| label25 = Nozzle
| data25 = {{#ifeq:{{{type|}}}|solid| {{{nozzle|}}} }}




| label30 = Mixture ratio
| data30 = {{#ifeq:{{{type|}}}|liquid| {{{mixture_ratio|}}} }}

| label31 = Cycle
| data31 = {{#ifeq:{{{type|}}}|liquid| {{{cycle|}}} }}

| label32 = Pumps
| data32 = {{#ifeq:{{{type|}}}|liquid| {{{pumps|}}} }}


| header40 = {{#if: {{{combustion_chamber|}}}{{{nozzle_ratio|}}} | Configuration }}

| data41 = {{{description|}}}

| label42 = Chamber
| data42 = {{{combustion_chamber|}}}

| label43 = Nozzle ratio
| data43 = {{{nozzle_ratio|}}}

| header50 = {{#if: {{{thrust(Vac)|}}}{{{thrust(SL)|}}}{{{thrust|}}}{{{thrust_at_altitude|}}}{{{thrust_to_weight|}}}{{{chamber_pressure|}}}{{{specific_impulse|}}}{{{specific_impulse_vacuum|}}}{{{specific_impulse_sea_level|}}}{{{total_impulse|}}}{{{burn_time|}}}{{{capacity|}}} | Performance }}

| label51 = Thrust
| data51 = {{{thrust|}}}

| label52 = {{#if: {{{thrust|}}} |     at altitude | Thrust, at altitude }}
| data52 = {{{thrust_at_altitude|}}}

| label53 = Thrust, vacuum
| data53 = {{{thrust(Vac)|}}}

| label54 = Thrust, sea-level
| data54 = {{{thrust(SL)|}}}

| label55 = Throttle range
| data55 = {{{throttle_range|}}}

| label60 = [[Thrust-to-weight ratio]]
| data60 = {{{thrust_to_weight|}}}

| label61 = Chamber [[pressure]]
| data61 = {{{chamber_pressure|}}}

| label62 = [[Specific impulse]]
| data62 = {{{specific_impulse|}}}

| label63 = [[Specific impulse]], vacuum
| data63 = {{{specific_impulse_vacuum|}}}

| label64 = [[Specific impulse]], sea-level
| data64 = {{{specific_impulse_sea_level|}}}

| label65 = [[Impulse (physics)|Total impulse]]
| data65 = {{{total_impulse|}}}

| label66 = [[Mass flow rate|Mass flow]]
| data66 = {{{mass_flow|}}}

| label70 = Burn time
| data70 = {{{burn_time|}}}

| label71 = Restarts
| data71 = {{{restarts|}}}

| label72 = {{#switch: {{lc:{{{type|}}}}}
| solid = [[Thrust vectoring]]
| liquid = [[Gimbaled thrust|Gimbal range]]
| hybrid = [[Thrust vectoring]]
| mono
| monopropellant = [[Gimbaled thrust|Gimbal range]]
}}
| data72 = {{{gimbal|}}}

| label73 = Propellant capacity
| data73 = {{{capacity|}}}

| header80 = {{#if: {{{dimensions|}}}{{{length|}}}{{{diameter|}}}{{{dry_weight|}}} | Dimensions }}

| label81 = Measurement
| data81 = {{{dimensions|}}}

| label82 = Length
| data82 = {{{length|}}}

| label83 = Diameter
| data83 = {{{diameter|}}}

| label84 = {{#switch: {{lc:{{{type|}}}}}
| solid = Empty mass
| liquid = Dry mass
| hybrid = Empty mass
| mono
| monopropellant = Dry mass
}}
| data84 = {{{dry_weight|}}}

| label85 = Gross mass
| data85 = {{{gross|}}}

| header90 = {{#if: {{{used_in|}}} | Used in }}
| data91 = {{{used_in|}}}

| header99 = {{{embedded|{{{module|}}}}}}

| header100 = {{#if: {{{references|}}}{{{notes|}}} | References }}

| label101 = References
| data101 = {{{references|}}}

| label102 = Notes
| data102 = {{{notes|}}}

}}{{main other|
{{#switch: {{lc:{{{country_of_origin|}}}}}
| britain|uk|united kingdom = [[Category:Rocket engines of the United Kingdom]]
| russia|russian|soviet|soviet union = [[Category:Rocket engines of the Soviet Union]]
| us|usa|united states = 
| france = 
}}{{#switch: {{lc:{{{type|}}}}}
| mono|monopropellant = [[Category:Monopropellant rocket engines]]
| solid = 
| liquid = 
| hybrid = 
}}
}}{{#invoke:Check for unknown parameters|check|unknown={{main other|[[Category:Pages using infobox rocket engine with unknown parameters|_VALUE_{{PAGENAME}}]]}}|preview=Page using [[Template:Infobox rocket engine]] with unknown parameter "_VALUE_"|ignoreblank=y| alt | associated | burn_time | capacity | caption | casing | chamber_pressure | combustion_chamber | core | country_of_origin | cycle | date | description | designer | diameter | dimensions | dry_weight | embedded | first_date | fuel | gimbal | grain | image | image_alt | image_size | imsize | last_date | length | manufacturer | mass_flow | mixture_ratio | module | name | notes | nozzle | nozzle_ratio | oxidiser | oxidizer | predecessor | pumps | purpose | references | restarts | specific_impulse | specific_impulse_sea_level | specific_impulse_vacuum | status | successor | throttle_range | thrust | thrust_at_altitude | thrust_to_weight | thrust(SL) | thrust(Vac) | total_impulse | type | used_in }}<noinclude>
{{documentation}}
<templatedata>
{
"params": {
"name": {
"label": "Name",
"description": "Name of the rocket engine",
"type": "string"
},
"image": {
"label": "Image",
"type": "wiki-file-name",
"description": "Filename for image of the rocket engine, do not include the \"File:\" or \"Image:\" prefix"
},
"alt": {},
"image_alt": {},
"caption": {
"label": "Caption",
"description": "Image caption",
"type": "string"
},
"country_of_origin": {
"label": "Country of origin",
"type": "string",
"description": "Country of origin"
},
"date": {},
"first_date": {
"label": "First flight date",
"description": "Date of the first flight, use {{Start date|YYYY|MM|DD|df=y}} ",
"example": "{{Start date|YYYY|MM|DD|df=y}} ",
"type": "string"
},
"last_date": {
"label": "Last flight date",
"description": "Date of the last flight, use {{End date|YYYY|MM|DD|df=y}} ",
"example": "{{End date|YYYY|MM|DD|df=y}}",
"type": "string"
},
"designer": {
"label": "Designer",
"description": "Designer of the engine, can be linked",
"type": "string"
},
"manufacturer": {
"label": "Manufacturer",
"description": "Manufacturer of the engine, can be linked, but do not link if the same as the designer",
"type": "string"
},
"purpose": {},
"associated": {
"label": "Associated launch vehicles",
"description": "List of launch vehicles this rocket engine is associated with",
"type": "string"
},
"predecessor": {
"label": "Predecessor ",
"description": "Predecessor rocket engine",
"type": "string"
},
"successor": {
"label": "Successor",
"description": "Successor rocket engine",
"type": "string"
},
"status": {},
"type": {
"label": "Type",
"description": "Type of rocket engine, use liquid, solid, hybrid or mono (for monopropellant) ",
"type": "string",
"suggestedvalues": [
"liquid",
"solid",
"hybrid",
"mono"
],
"required": true
},
"fuel": {
"label": "Fuel",
"description": "Type of fuel used",
"type": "string"
},
"oxidizer": {
"aliases": [
"oxidiser"
],
"label": "Oxidizer",
"description": "Type of oxidizer used",
"type": "string"
},
"grain": {},
"core": {},
"casing": {},
"nozzle": {},
"mixture_ratio": {},
"cycle": {},
"pumps": {},
"combustion_chamber": {},
"nozzle_ratio": {},
"description": {},
"thrust(Vac)": {
"label": "Thrust, vacuum",
"description": "Thrust of the engine, in vacuum, use {{cvt|VALUEHERE|kN}}",
"example": "{{cvt|VALUEHERE|kN}}",
"type": "string"
},
"thrust(SL)": {
"label": "Thrust, sea level",
"description": "Thrust of the engine, at sea level, use {{cvt|VALUEHERE|kN}}",
"example": "{{cvt|VALUEHERE|kN}}",
"type": "string"
},
"thrust": {
"label": "Thrust",
"deprecated": "Use Thrust, vacuum or Thrust, sea level"
},
"thrust_at_altitude": {},
"thrust_to_weight": {},
"chamber_pressure": {},
"specific_impulse": {
"label": "Specific impulse",
"deprecated": "Use Specific impulse, vacuum or Specific impulse, sea level"
},
"specific_impulse_vacuum": {
"label": "Specific impulse, vacuum",
"description": "Specific impulse of the engine, in vacuum, use {{cvt|VALUEHERE|isp}}",
"example": "{{cvt|VALUEHERE|isp}}",
"type": "string"
},
"specific_impulse_sea_level": {
"label": "Specific impulse, vacuum",
"description": "Specific impulse of the engine, at sea level, use {{cvt|VALUEHERE|isp}}",
"example": "{{cvt|VALUEHERE|isp}}"
},
"total_impulse": {},
"burn_time": {
"label": "Burn time",
"description": "The length of time the engine burns normally, in seconds",
"example": "NNN seconds",
"type": "string"
},
"capacity": {},
"throttle_range": {},
"mass_flow": {},
"restarts": {
"label": "Restarts",
"description": "How many times the engine can be restarted, leave blank if not restartable"
},
"gimbal": {
"label": "Gimbal range",
"description": "Gimbal range in °, leave blank if none-->",
"example": "NN°",
"type": "string"
},
"dimensions": {},
"length": {
"label": "Length",
"description": "Length of the engine, in metres, use {{cvt|VALUE|m}}",
"example": "{{cvt|VALUE|m}}",
"type": "string"
},
"diameter": {
"label": "Diameter",
"description": "Diameter of the engine at widest part (typically nozzle tip), in metres, use {{cvt|VALUE|m}}",
"example": "{{cvt|VALUE|m}}",
"type": "string"
},
"dry_weight": {
"label": "Dry weight",
"description": "Mass of unfueled rocket engine in kilograms, use {{cvt|MASS|kg}}",
"example": "{{cvt|MASS|kg}}",
"type": "string"
},
"used_in": {},
"embedded": {},
"module": {},
"references": {},
"notes": {},
"image_size": {
"aliases": [
"imsize"
],
"label": "Image size",
"description": "Image size in pixels",
"type": "string"
}
},
"format": "{{_\n| __________________________ = _\n}}",
"paramOrder": [
"name",
"image",
"image_size",
"alt",
"image_alt",
"caption",
"country_of_origin",
"date",
"first_date",
"last_date",
"designer",
"manufacturer",
"purpose",
"associated",
"predecessor",
"successor",
"status",
"type",
"fuel",
"oxidizer",
"grain",
"core",
"casing",
"nozzle",
"mixture_ratio",
"cycle",
"pumps",
"combustion_chamber",
"nozzle_ratio",
"description",
"thrust(Vac)",
"thrust(SL)",
"thrust",
"thrust_at_altitude",
"thrust_to_weight",
"chamber_pressure",
"specific_impulse",
"specific_impulse_vacuum",
"specific_impulse_sea_level",
"total_impulse",
"burn_time",
"capacity",
"throttle_range",
"mass_flow",
"restarts",
"gimbal",
"dimensions",
"length",
"diameter",
"dry_weight",
"used_in",
"embedded",
"module",
"references",
"notes"
]
}
</templatedata></noinclude>

Template:Infobox rocket engine - Revision history

>RickyCourtney: Add params