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	<id>https://www.vigyanwiki.in/index.php?action=history&amp;feed=atom&amp;title=Template%3AInfobox_rocket_engine</id>
	<title>Template:Infobox rocket engine - Revision history</title>
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	<updated>2026-06-12T14:31:10Z</updated>
	<subtitle>Revision history for this page on the wiki</subtitle>
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	<entry>
		<id>https://www.vigyanwiki.in/index.php?title=Template:Infobox_rocket_engine&amp;diff=78042&amp;oldid=prev</id>
		<title>Indicwiki: 1 revision imported from :alpha:Template:Infobox_rocket_engine</title>
		<link rel="alternate" type="text/html" href="https://www.vigyanwiki.in/index.php?title=Template:Infobox_rocket_engine&amp;diff=78042&amp;oldid=prev"/>
		<updated>2023-02-03T09:35:54Z</updated>

		<summary type="html">&lt;p&gt;1 revision imported from &lt;a href=&quot;https://alpha.indicwiki.in/index.php?title=Template:Infobox_rocket_engine&quot; class=&quot;extiw&quot; title=&quot;alpha:Template:Infobox rocket engine&quot;&gt;alpha:Template:Infobox_rocket_engine&lt;/a&gt;&lt;/p&gt;
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				&lt;td colspan=&quot;1&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&quot;1&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;Revision as of 15:05, 3 February 2023&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-notice&quot; lang=&quot;en-GB&quot;&gt;&lt;div class=&quot;mw-diff-empty&quot;&gt;(No difference)&lt;/div&gt;
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		<author><name>Indicwiki</name></author>
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	<entry>
		<id>https://www.vigyanwiki.in/index.php?title=Template:Infobox_rocket_engine&amp;diff=78041&amp;oldid=prev</id>
		<title>alpha&gt;Indicwiki: Created page with &quot;{{Infobox  | title          = &lt;includeonly&gt;{{{name|{{PAGENAMEBASE}}}}}&lt;/includeonly&gt;  | headerstyle    = background-color:#FFDEAD  | image          = {{#invoke:InfoboxImage|In...&quot;</title>
		<link rel="alternate" type="text/html" href="https://www.vigyanwiki.in/index.php?title=Template:Infobox_rocket_engine&amp;diff=78041&amp;oldid=prev"/>
		<updated>2023-01-27T05:34:42Z</updated>

		<summary type="html">&lt;p&gt;Created page with &amp;quot;{{Infobox  | title          = &amp;lt;includeonly&amp;gt;{{{name|{{PAGENAMEBASE}}}}}&amp;lt;/includeonly&amp;gt;  | headerstyle    = background-color:#FFDEAD  | image          = {{#invoke:InfoboxImage|In...&amp;quot;&lt;/p&gt;
&lt;p&gt;&lt;b&gt;New page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;{{Infobox&lt;br /&gt;
 | title          = &amp;lt;includeonly&amp;gt;{{{name|{{PAGENAMEBASE}}}}}&amp;lt;/includeonly&amp;gt;&lt;br /&gt;
 | headerstyle    = background-color:#FFDEAD&lt;br /&gt;
 | image          = {{#invoke:InfoboxImage|InfoboxImage|image={{{image|}}}|size={{{image_size|{{{imsize|}}}}}}|sizedefault=frameless|upright=1.13|alt={{{alt|{{{image_alt|}}}}}}}}&lt;br /&gt;
 | caption        = {{{caption|}}}&lt;br /&gt;
&lt;br /&gt;
 | label1 = Country of origin&lt;br /&gt;
 | data1 = {{{country_of_origin|}}}&lt;br /&gt;
&lt;br /&gt;
 | label2 = Date&lt;br /&gt;
 | data2 = {{{date|}}}&lt;br /&gt;
&lt;br /&gt;
 | label3 = First flight&lt;br /&gt;
 | data3 = {{{first_date|}}}&lt;br /&gt;
&lt;br /&gt;
 | label4 = Last flight&lt;br /&gt;
 | data4 = {{{last_date|}}}&lt;br /&gt;
&lt;br /&gt;
 | label5 = Designer&lt;br /&gt;
 | data5 = {{{designer|}}}&lt;br /&gt;
&lt;br /&gt;
 | label10 = Manufacturer&lt;br /&gt;
 | data10 = {{{manufacturer|}}}&lt;br /&gt;
&lt;br /&gt;
 | label11 = Application&lt;br /&gt;
 | data11 = {{{purpose|}}}&lt;br /&gt;
&lt;br /&gt;
 | label12 = Associated {{abbr|LV|launch vehicle}}&lt;br /&gt;
 | data12 = {{{associated|}}}&lt;br /&gt;
&lt;br /&gt;
 | label13 = Predecessor&lt;br /&gt;
 | data13 = {{{predecessor|}}}&lt;br /&gt;
&lt;br /&gt;
 | label14 = Successor&lt;br /&gt;
 | data14 = {{{successor|}}}&lt;br /&gt;
&lt;br /&gt;
 | label15 = Status&lt;br /&gt;
 | data15 = {{{status|}}}&lt;br /&gt;
&lt;br /&gt;
 | header20 = {{#switch: {{lc:{{{type|}}}}}&lt;br /&gt;
   | solid          = [[Solid-fuel rocket|Solid-fuel motor]]&lt;br /&gt;
   | liquid         = [[Liquid-propellant rocket|Liquid-fuel engine]]&lt;br /&gt;
   | hybrid         = [[Hybrid rocket|Hybrid engine]]&lt;br /&gt;
   | mono|monopropellant = {{{fuel|}}} [[monopropellant]]&lt;br /&gt;
   | #default       = {{{type|}}}&lt;br /&gt;
 }}&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!-- start section for type = solid, liquid, or hybrid parameters --&amp;gt;&lt;br /&gt;
 | label21 = Propellant&lt;br /&gt;
 | data21 = {{#switch: {{lc:{{{type|}}}}}&lt;br /&gt;
   | solid&lt;br /&gt;
   | liquid&lt;br /&gt;
   | hybrid  = {{#if: {{{oxidizer|}}}{{{oxidiser|}}} | {{{oxidizer|{{{oxidiser|}}}}}} / }} {{{fuel|}}}&lt;br /&gt;
  }}&lt;br /&gt;
&amp;lt;!-- end section for type = solid, liquid, or hybrid parameters --&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!-- start section for type = solid parameters --&amp;gt;&lt;br /&gt;
 | label22 = Grain&lt;br /&gt;
 | data22 = {{#ifeq:{{{type|}}}|solid| {{{grain|}}} }}&lt;br /&gt;
&lt;br /&gt;
 | label23 = Core&lt;br /&gt;
 | data23 = {{#ifeq:{{{type|}}}|solid| {{{core|}}} }}&lt;br /&gt;
&lt;br /&gt;
 | label24 = Casing&lt;br /&gt;
 | data24 = {{#ifeq:{{{type|}}}|solid| {{{casing|}}} }}&lt;br /&gt;
&lt;br /&gt;
 | label25 = Nozzle&lt;br /&gt;
 | data25 = {{#ifeq:{{{type|}}}|solid| {{{nozzle|}}} }}&lt;br /&gt;
&amp;lt;!-- end section for type = solid parameters --&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!-- start section for type = liquid parameters --&amp;gt;&lt;br /&gt;
 | label30 = Mixture ratio&lt;br /&gt;
 | data30 = {{#ifeq:{{{type|}}}|liquid| {{{mixture_ratio|}}} }}&lt;br /&gt;
&lt;br /&gt;
 | label31 = Cycle&lt;br /&gt;
 | data31 = {{#ifeq:{{{type|}}}|liquid| {{{cycle|}}} }}&lt;br /&gt;
&lt;br /&gt;
 | label32 = Pumps&lt;br /&gt;
 | data32 = {{#ifeq:{{{type|}}}|liquid| {{{pumps|}}} }}&lt;br /&gt;
&amp;lt;!-- end section for type = liquid parameters --&amp;gt;&lt;br /&gt;
&lt;br /&gt;
 | header40 = {{#if: {{{combustion_chamber|}}}{{{nozzle_ratio|}}} | Configuration }}&lt;br /&gt;
&lt;br /&gt;
 | data41 = {{{description|}}}&lt;br /&gt;
&lt;br /&gt;
 | label42 = Chamber&lt;br /&gt;
 | data42 = {{{combustion_chamber|}}}&lt;br /&gt;
&lt;br /&gt;
 | label43 = Nozzle ratio&lt;br /&gt;
 | data43 = {{{nozzle_ratio|}}}&lt;br /&gt;
&lt;br /&gt;
 | 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 }}&lt;br /&gt;
&lt;br /&gt;
 | label51 = Thrust&lt;br /&gt;
 | data51 = {{{thrust|}}}&lt;br /&gt;
&lt;br /&gt;
 | label52 = {{#if: {{{thrust|}}} | &amp;amp;nbsp;&amp;amp;nbsp;&amp;amp;nbsp;&amp;amp;nbsp;at altitude | Thrust, at altitude }}&lt;br /&gt;
 | data52 = {{{thrust_at_altitude|}}}&lt;br /&gt;
&lt;br /&gt;
 | label53 = Thrust, vacuum&lt;br /&gt;
 | data53 = {{{thrust(Vac)|}}}&lt;br /&gt;
&lt;br /&gt;
 | label54 = Thrust, sea-level&lt;br /&gt;
 | data54 = {{{thrust(SL)|}}}&lt;br /&gt;
&lt;br /&gt;
 | label55 = Throttle range&lt;br /&gt;
 | data55 = {{{throttle_range|}}}&lt;br /&gt;
&lt;br /&gt;
 | label60 = [[Thrust-to-weight ratio]]&lt;br /&gt;
 | data60 = {{{thrust_to_weight|}}}&lt;br /&gt;
&lt;br /&gt;
 | label61 = Chamber [[pressure]]&lt;br /&gt;
 | data61 = {{{chamber_pressure|}}}&lt;br /&gt;
&lt;br /&gt;
 | label62 = [[Specific impulse]]&lt;br /&gt;
 | data62 = {{{specific_impulse|}}}&lt;br /&gt;
&lt;br /&gt;
 | label63 = [[Specific impulse]], vacuum&lt;br /&gt;
 | data63 = {{{specific_impulse_vacuum|}}}&lt;br /&gt;
&lt;br /&gt;
 | label64 = [[Specific impulse]], sea-level&lt;br /&gt;
 | data64 = {{{specific_impulse_sea_level|}}}&lt;br /&gt;
&lt;br /&gt;
 | label65 = [[Impulse (physics)|Total impulse]]&lt;br /&gt;
 | data65 = {{{total_impulse|}}}&lt;br /&gt;
&lt;br /&gt;
 | label66 = [[Mass flow rate|Mass flow]]&lt;br /&gt;
 | data66 = {{{mass_flow|}}}&lt;br /&gt;
&lt;br /&gt;
 | label70 = Burn time&lt;br /&gt;
 | data70 = {{{burn_time|}}}&lt;br /&gt;
&lt;br /&gt;
 | label71 = Restarts&lt;br /&gt;
 | data71 = {{{restarts|}}}&lt;br /&gt;
&lt;br /&gt;
 | label72 = {{#switch: {{lc:{{{type|}}}}}&lt;br /&gt;
   | solid  = [[Thrust vectoring]]&lt;br /&gt;
   | liquid = [[Gimbaled thrust|Gimbal range]]&lt;br /&gt;
   | hybrid = [[Thrust vectoring]]&lt;br /&gt;
   | mono&lt;br /&gt;
   | monopropellant = [[Gimbaled thrust|Gimbal range]]&lt;br /&gt;
 }}&lt;br /&gt;
&lt;br /&gt;
 | data72 = {{{gimbal|}}}&lt;br /&gt;
&lt;br /&gt;
 | label73 = Propellant capacity&lt;br /&gt;
 | data73 = {{{capacity|}}}&lt;br /&gt;
&lt;br /&gt;
 | header80 = {{#if: {{{dimensions|}}}{{{length|}}}{{{diameter|}}}{{{dry_weight|}}} | Dimensions }}&lt;br /&gt;
&lt;br /&gt;
 | label81 = Measurement&lt;br /&gt;
 | data81 = {{{dimensions|}}}&lt;br /&gt;
&lt;br /&gt;
 | label82 = Length&lt;br /&gt;
 | data82 = {{{length|}}}&lt;br /&gt;
&lt;br /&gt;
 | label83 = Diameter&lt;br /&gt;
 | data83 = {{{diameter|}}}&lt;br /&gt;
&lt;br /&gt;
 | label84 = Dry weight&lt;br /&gt;
 | data84 = {{{dry_weight|}}}&lt;br /&gt;
 | header90 = {{#if: {{{used_in|}}} | Used in }}&lt;br /&gt;
 | data91 = {{{used_in|}}}&lt;br /&gt;
&lt;br /&gt;
 | header99 = {{{embedded|{{{module|}}}}}}&lt;br /&gt;
&lt;br /&gt;
 | header100 = {{#if: {{{references|}}}{{{notes|}}} | References }}&lt;br /&gt;
&lt;br /&gt;
 | label101 = References&lt;br /&gt;
 | data101 = {{{references|}}}&lt;br /&gt;
&lt;br /&gt;
 | label102 = Notes&lt;br /&gt;
 | data102 = {{{notes|}}}&lt;br /&gt;
&lt;br /&gt;
}}{{main other|&lt;br /&gt;
  {{#switch: {{lc:{{{country_of_origin|}}}}}&lt;br /&gt;
   | britain|uk|united kingdom = [[Category:Rocket engines of the United Kingdom]]&lt;br /&gt;
   | russia|russian|soviet|soviet union = [[Category:Rocket engines of the Soviet Union]]&lt;br /&gt;
   | us|usa|united states = &amp;lt;!--Does not currently exist--&amp;gt;&lt;br /&gt;
   | france         = &amp;lt;!--Does not currently exist--&amp;gt;&lt;br /&gt;
 }}{{#switch: {{lc:{{{type|}}}}}&lt;br /&gt;
   | mono|monopropellant = [[Category:Monopropellant rocket engines]]&lt;br /&gt;
   | solid          = &amp;lt;!--Does not currently exist--&amp;gt;&lt;br /&gt;
   | liquid         = &amp;lt;!--Does not currently exist--&amp;gt;&lt;br /&gt;
   | hybrid         = &amp;lt;!--Does not currently exist--&amp;gt;&lt;br /&gt;
 }}&lt;br /&gt;
}}{{#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 &amp;quot;_VALUE_&amp;quot;|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 }}&amp;lt;noinclude&amp;gt;&lt;br /&gt;
{{Documentation}}&lt;br /&gt;
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		<author><name>alpha&gt;Indicwiki</name></author>
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