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	<updated>2026-06-10T09:17:55Z</updated>
	<subtitle>User contributions</subtitle>
	<generator>MediaWiki 1.34.2</generator>
	<entry>
		<id>https://blackwiki.org/index.php?title=Template:Infobox_rocket_engine/doc&amp;diff=6350450</id>
		<title>Template:Infobox rocket engine/doc</title>
		<link rel="alternate" type="text/html" href="https://blackwiki.org/index.php?title=Template:Infobox_rocket_engine/doc&amp;diff=6350450"/>
		<updated>2021-02-11T01:33:05Z</updated>

		<summary type="html">&lt;p&gt;163.158.132.63: Added mass flow&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{Documentation subpage}}&lt;br /&gt;
&amp;lt;!-- PLEASE ADD CATEGORIES AND INTERWIKIS AT THE BOTTOM OF THIS PAGE --&amp;gt;&lt;br /&gt;
{{TOCright}}&lt;br /&gt;
This template is intended for use on articles about '''[[rocket engine]]s''' and '''[[spacecraft propulsion]]'''. See [[SpaceX Raptor|example]] for result.&lt;br /&gt;
&lt;br /&gt;
== Empty premade templates ==&lt;br /&gt;
&lt;br /&gt;
{| style=&amp;quot;background:transparent;&amp;quot;&lt;br /&gt;
| width=50% style=&amp;quot;vertical-align:top;&amp;quot; |&lt;br /&gt;
;Liquid engines&lt;br /&gt;
&amp;lt;pre style=&amp;quot;overflow:auto;&amp;quot;&amp;gt;&lt;br /&gt;
{{Infobox rocket engine&lt;br /&gt;
|name            =&lt;br /&gt;
|image           =&lt;br /&gt;
|image_size      =&lt;br /&gt;
|caption         =&lt;br /&gt;
|country_of_origin=&lt;br /&gt;
|date            =&lt;br /&gt;
|first_date      =&lt;br /&gt;
|last_date       =&lt;br /&gt;
|designer        =&lt;br /&gt;
|manufacturer    =&lt;br /&gt;
|purpose         =&lt;br /&gt;
|associated      =&lt;br /&gt;
|predecessor     =&lt;br /&gt;
|successor       =&lt;br /&gt;
|status          =&lt;br /&gt;
&lt;br /&gt;
|type            =liquid&lt;br /&gt;
|oxidiser        =&lt;br /&gt;
|fuel            =&lt;br /&gt;
|mixture_ratio   =&lt;br /&gt;
|cycle           =&lt;br /&gt;
|pumps           =&lt;br /&gt;
&lt;br /&gt;
|description     =&lt;br /&gt;
|combustion_chamber=&lt;br /&gt;
|nozzle_ratio    =&lt;br /&gt;
&lt;br /&gt;
|thrust          =&lt;br /&gt;
|thrust_at_altitude=&lt;br /&gt;
|thrust(Vac)     =&amp;lt;!--if throttle range &amp;gt;100%, specify corresponding throttle--&amp;gt;&lt;br /&gt;
|thrust(SL)      =&lt;br /&gt;
|throttle_range  =&amp;lt;!--leave blank if no throttle--&amp;gt;&lt;br /&gt;
|thrust_to_weight=&lt;br /&gt;
|chamber_pressure=&lt;br /&gt;
|specific_impulse=&lt;br /&gt;
|specific_impulse_vacuum=&lt;br /&gt;
|specific_impulse_sea_level=&lt;br /&gt;
|total_impulse   =&lt;br /&gt;
|mass_flow       =&lt;br /&gt;
|burn_time       =&lt;br /&gt;
|restarts        =&amp;lt;!--leave blank if not restartable--&amp;gt;&lt;br /&gt;
|gimbal          =&amp;lt;!--gimbal range in °, leave blank if none--&amp;gt;&lt;br /&gt;
|capacity        =&lt;br /&gt;
&lt;br /&gt;
|dimensions      =&lt;br /&gt;
|length          =&lt;br /&gt;
|diameter        =&lt;br /&gt;
|dry_weight      =&lt;br /&gt;
&lt;br /&gt;
|used_in         =&lt;br /&gt;
&lt;br /&gt;
|references      =&lt;br /&gt;
|notes           =&lt;br /&gt;
}}&lt;br /&gt;
&amp;lt;/pre&amp;gt;&lt;br /&gt;
| width=50% style=&amp;quot;vertical-align:top;&amp;quot; |&lt;br /&gt;
;Solid engines&lt;br /&gt;
&amp;lt;pre style=&amp;quot;overflow:auto;&amp;quot;&amp;gt;&lt;br /&gt;
{{Infobox rocket engine&lt;br /&gt;
|name            =&lt;br /&gt;
|image           =&lt;br /&gt;
|image_size      =&lt;br /&gt;
|caption         =&lt;br /&gt;
|country_of_origin=&lt;br /&gt;
|date            =&lt;br /&gt;
|first_date      =&lt;br /&gt;
|last_date       =&lt;br /&gt;
|designer        =&lt;br /&gt;
|manufacturer    =&lt;br /&gt;
|purpose         =&lt;br /&gt;
|associated      =&lt;br /&gt;
|predecessor     =&lt;br /&gt;
|successor       =&lt;br /&gt;
|status          =&lt;br /&gt;
&lt;br /&gt;
|type            =solid&lt;br /&gt;
|oxidiser        =&lt;br /&gt;
|fuel            =&lt;br /&gt;
|grain           =&lt;br /&gt;
|core            =&lt;br /&gt;
|casing          =&lt;br /&gt;
|nozzle          =&lt;br /&gt;
&lt;br /&gt;
|description     =&lt;br /&gt;
|combustion_chamber=&lt;br /&gt;
|nozzle_ratio    =&lt;br /&gt;
&lt;br /&gt;
|thrust          =&lt;br /&gt;
|thrust_at_altitude=&lt;br /&gt;
|thrust(Vac)     =&lt;br /&gt;
|thrust(SL)      =&lt;br /&gt;
|thrust_to_weight=&lt;br /&gt;
|chamber_pressure=&lt;br /&gt;
|specific_impulse=&lt;br /&gt;
|specific_impulse_vacuum=&lt;br /&gt;
|specific_impulse_sea_level=&lt;br /&gt;
|total_impulse   =&lt;br /&gt;
|mass_flow       =&lt;br /&gt;
|burn_time       =&lt;br /&gt;
|gimbal          =&amp;lt;!--gimbal range in °, or other TVC method, leave blank if none--&amp;gt;&lt;br /&gt;
|capacity        =&lt;br /&gt;
&lt;br /&gt;
|dimensions      =&lt;br /&gt;
|length          =&lt;br /&gt;
|diameter        =&lt;br /&gt;
|dry_weight      =&lt;br /&gt;
&lt;br /&gt;
|used_in         =&lt;br /&gt;
&lt;br /&gt;
|references      =&lt;br /&gt;
|notes           =&lt;br /&gt;
}}&lt;br /&gt;
&amp;lt;/pre&amp;gt;&lt;br /&gt;
|-&lt;br /&gt;
| width=50% style=&amp;quot;vertical-align:top;&amp;quot; |&lt;br /&gt;
;Hybrid engines&lt;br /&gt;
&amp;lt;pre style=&amp;quot;overflow:auto;&amp;quot;&amp;gt;&lt;br /&gt;
{{Infobox rocket engine&lt;br /&gt;
|name            =&lt;br /&gt;
|image           =&lt;br /&gt;
|image_size      =&lt;br /&gt;
|caption         =&lt;br /&gt;
|country_of_origin=&lt;br /&gt;
|date            =&lt;br /&gt;
|first_date      =&lt;br /&gt;
|last_date       =&lt;br /&gt;
|designer        =&lt;br /&gt;
|manufacturer    =&lt;br /&gt;
|purpose         =&lt;br /&gt;
|associated      =&lt;br /&gt;
|predecessor     =&lt;br /&gt;
|successor       =&lt;br /&gt;
|status          =&lt;br /&gt;
&lt;br /&gt;
|type            =hybrid&lt;br /&gt;
|oxidiser        =&lt;br /&gt;
|fuel            =&lt;br /&gt;
&lt;br /&gt;
|description     =&lt;br /&gt;
|combustion_chamber=&lt;br /&gt;
|nozzle_ratio    =&lt;br /&gt;
&lt;br /&gt;
|thrust          =&lt;br /&gt;
|thrust_at_altitude=&lt;br /&gt;
|thrust(Vac)     =&amp;lt;!--if throttle range &amp;gt;100%, specify corresponding throttle--&amp;gt;&lt;br /&gt;
|thrust(SL)      =&lt;br /&gt;
|throttle_range  =&amp;lt;!--leave blank if no throttle--&amp;gt;&lt;br /&gt;
|thrust_to_weight=&lt;br /&gt;
|chamber_pressure=&lt;br /&gt;
|specific_impulse=&lt;br /&gt;
|specific_impulse_vacuum=&lt;br /&gt;
|specific_impulse_sea_level=&lt;br /&gt;
|total_impulse   =&lt;br /&gt;
|mass_flow       =&lt;br /&gt;
|burn_time       =&lt;br /&gt;
|restarts        =&amp;lt;!--leave blank if not restartable--&amp;gt;&lt;br /&gt;
|gimbal          =&amp;lt;!--gimbal range in °, leave blank if none--&amp;gt;&lt;br /&gt;
|capacity        =&lt;br /&gt;
&lt;br /&gt;
|dimensions      =&lt;br /&gt;
|length          =&lt;br /&gt;
|diameter        =&lt;br /&gt;
|dry_weight      =&lt;br /&gt;
&lt;br /&gt;
|used_in         =&lt;br /&gt;
&lt;br /&gt;
|references      =&lt;br /&gt;
|notes           =&lt;br /&gt;
}}&lt;br /&gt;
&amp;lt;/pre&amp;gt;&lt;br /&gt;
| width=50% style=&amp;quot;vertical-align:top;&amp;quot; |&lt;br /&gt;
;Monopropellant engines&lt;br /&gt;
&amp;lt;pre style=&amp;quot;overflow:auto;&amp;quot;&amp;gt;&lt;br /&gt;
{{Infobox rocket engine&lt;br /&gt;
|name            =&lt;br /&gt;
|image           =&lt;br /&gt;
|image_size      =&lt;br /&gt;
|caption         =&lt;br /&gt;
|country_of_origin=&lt;br /&gt;
|date            =&lt;br /&gt;
|first_date      =&lt;br /&gt;
|last_date       =&lt;br /&gt;
|designer        =&lt;br /&gt;
|manufacturer    =&lt;br /&gt;
|purpose         =&lt;br /&gt;
|associated      =&lt;br /&gt;
|predecessor     =&lt;br /&gt;
|successor       =&lt;br /&gt;
|status          =&lt;br /&gt;
&lt;br /&gt;
|type            =mono&lt;br /&gt;
|fuel            =&lt;br /&gt;
&lt;br /&gt;
|description     =&lt;br /&gt;
|combustion_chamber=&lt;br /&gt;
|nozzle_ratio    =&lt;br /&gt;
&lt;br /&gt;
|thrust          =&lt;br /&gt;
|thrust_at_altitude=&lt;br /&gt;
|thrust(Vac)     =&amp;lt;!--if throttle range &amp;gt;100%, specify corresponding throttle--&amp;gt;&lt;br /&gt;
|thrust(SL)      =&lt;br /&gt;
|throttle_range  =&amp;lt;!--leave blank if no throttle--&amp;gt;&lt;br /&gt;
|thrust_to_weight=&lt;br /&gt;
|chamber_pressure=&lt;br /&gt;
|specific_impulse=&lt;br /&gt;
|specific_impulse_vacuum=&lt;br /&gt;
|specific_impulse_sea_level=&lt;br /&gt;
|total_impulse   =&lt;br /&gt;
|mass_flow       =&lt;br /&gt;
|burn_time       =&lt;br /&gt;
|restarts        =&amp;lt;!--leave blank if not restartable--&amp;gt;&lt;br /&gt;
|gimbal          =&amp;lt;!--gimbal range in °, leave blank if none--&amp;gt;&lt;br /&gt;
|capacity        =&lt;br /&gt;
&lt;br /&gt;
|dimensions      =&lt;br /&gt;
|length          =&lt;br /&gt;
|diameter        =&lt;br /&gt;
|dry_weight      =&lt;br /&gt;
&lt;br /&gt;
|used_in         =&lt;br /&gt;
&lt;br /&gt;
|references      =&lt;br /&gt;
|notes           =&lt;br /&gt;
}}&lt;br /&gt;
&amp;lt;/pre&amp;gt;&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
== Parameters ==&lt;br /&gt;
* '''name'''&lt;br /&gt;
&lt;br /&gt;
=== Image ===&lt;br /&gt;
* '''image'''&lt;br /&gt;
* '''caption'''&lt;br /&gt;
* '''imsize'''&lt;br /&gt;
&lt;br /&gt;
=== Origins ===&lt;br /&gt;
* '''country of origin'''&lt;br /&gt;
* '''date'''&lt;br /&gt;
* '''first flight'''&lt;br /&gt;
* '''last flight'''&lt;br /&gt;
&lt;br /&gt;
* '''designer'''&lt;br /&gt;
* '''manufacturer'''&lt;br /&gt;
&lt;br /&gt;
* '''purpose''' - &amp;quot;booster&amp;quot;, &amp;quot;apogee kick&amp;quot;, etc.&lt;br /&gt;
&lt;br /&gt;
* '''predecessor'''&lt;br /&gt;
* '''successor'''&lt;br /&gt;
* '''associated'''&lt;br /&gt;
* '''status'''&lt;br /&gt;
&lt;br /&gt;
=== Type ===&lt;br /&gt;
* '''type'''&lt;br /&gt;
** solid&lt;br /&gt;
** liquid&lt;br /&gt;
** hybrid&lt;br /&gt;
** mono / monopropellant&lt;br /&gt;
&lt;br /&gt;
==== Solids ====&lt;br /&gt;
* '''oxidiser''' / '''fuel'''&lt;br /&gt;
* '''grain'''&lt;br /&gt;
* '''core'''&lt;br /&gt;
* '''casing'''&lt;br /&gt;
* '''nozzle'''&lt;br /&gt;
&lt;br /&gt;
==== liquid ====&lt;br /&gt;
* '''oxidiser''' / '''fuel'''&lt;br /&gt;
* '''mixture_ratio'''&lt;br /&gt;
* '''cycle'''&lt;br /&gt;
* '''pumps'''&lt;br /&gt;
&lt;br /&gt;
==== hybrid ====&lt;br /&gt;
* '''oxidiser''' / '''fuel'''&lt;br /&gt;
&lt;br /&gt;
==== monopropellant ====&lt;br /&gt;
* '''fuel'''&lt;br /&gt;
&lt;br /&gt;
==== others ====&lt;br /&gt;
Just use the &amp;quot;type&amp;quot; and &amp;quot;description&amp;quot; fields.&lt;br /&gt;
&lt;br /&gt;
=== Configuration ===&lt;br /&gt;
* '''description'''&lt;br /&gt;
* '''combustion_chamber'''&lt;br /&gt;
* '''nozzle_ratio'''&lt;br /&gt;
&lt;br /&gt;
=== Performance ===&lt;br /&gt;
* '''thrust'''&lt;br /&gt;
* '''thrust(Vac)'''&lt;br /&gt;
* '''thrust(SL)'''&lt;br /&gt;
* '''thrust_at_altitude'''&lt;br /&gt;
* '''throttle_range'''&lt;br /&gt;
* '''thrust_to_weight_ratio'''&lt;br /&gt;
&lt;br /&gt;
* '''specific_impulse'''&lt;br /&gt;
* '''specific_impulse_vacuum'''&lt;br /&gt;
* '''specific_impulse_sea_level'''&lt;br /&gt;
* '''total_impulse'''&lt;br /&gt;
&lt;br /&gt;
* '''mass_flow'''&lt;br /&gt;
&lt;br /&gt;
* '''burn_time'''&lt;br /&gt;
* '''restarts'''&lt;br /&gt;
* '''gimbal'''&lt;br /&gt;
* '''capacity'''&lt;br /&gt;
: tankage&lt;br /&gt;
&lt;br /&gt;
=== Dimensions ===&lt;br /&gt;
* '''dimensions''' - use for overall description, otherwise use more specific fields&lt;br /&gt;
* '''length'''&lt;br /&gt;
* '''diameter'''&lt;br /&gt;
* '''dry_weight'''&lt;br /&gt;
&lt;br /&gt;
=== Applications ===&lt;br /&gt;
* '''used_in'''&lt;br /&gt;
&lt;br /&gt;
=== References ===&lt;br /&gt;
* '''references'''&lt;br /&gt;
* '''notes'''&lt;br /&gt;
&lt;br /&gt;
{{Spaceflight infoboxes}}&lt;br /&gt;
&lt;br /&gt;
&amp;lt;includeonly&amp;gt;{{Sandbox other||&lt;br /&gt;
&amp;lt;!-- CATEGORIES HERE, THANKS --&amp;gt;&lt;br /&gt;
[[Category:Rocketry templates|Rocket engine]]&lt;br /&gt;
[[Category:Spaceflight infobox templates|Rocket engine]]&lt;br /&gt;
[[Category:Technology and applied science infobox templates|Rocket engine]]&lt;br /&gt;
}}&amp;lt;/includeonly&amp;gt;&lt;/div&gt;</summary>
		<author><name>163.158.132.63</name></author>
		
	</entry>
	<entry>
		<id>https://blackwiki.org/index.php?title=Template:Infobox_rocket_engine&amp;diff=6350415</id>
		<title>Template:Infobox rocket engine</title>
		<link rel="alternate" type="text/html" href="https://blackwiki.org/index.php?title=Template:Infobox_rocket_engine&amp;diff=6350415"/>
		<updated>2021-02-11T01:31:29Z</updated>

		<summary type="html">&lt;p&gt;163.158.132.63: Added mass flow&lt;/p&gt;
&lt;hr /&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 L/V&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 (vac.)&lt;br /&gt;
 | data53 = {{{thrust(Vac)|}}}&lt;br /&gt;
&lt;br /&gt;
 | label54 = Thrust (SL)&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|''I''&amp;lt;sub&amp;gt;sp&amp;lt;/sub&amp;gt;]] (vac.)&lt;br /&gt;
 | data63 = {{{specific_impulse_vacuum|}}}&lt;br /&gt;
&lt;br /&gt;
 | label64 = [[Specific impulse|''I''&amp;lt;sub&amp;gt;sp&amp;lt;/sub&amp;gt;]] (SL)&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;
}}&amp;lt;noinclude&amp;gt;&lt;br /&gt;
{{Documentation}}&lt;br /&gt;
&amp;lt;/noinclude&amp;gt;&lt;/div&gt;</summary>
		<author><name>163.158.132.63</name></author>
		
	</entry>
</feed>