View source for Template:Infobox rocket engine

{{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 L/V
 | 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|}}}
 }}

<!-- start section for type = solid, liquid, or hybrid parameters -->
 | label21 = Propellant
 | data21 = {{#switch: {{lc:{{{type|}}}}}
   | solid
   | liquid
   | hybrid  = {{#if: {{{oxidizer|}}}{{{oxidiser|}}} | {{{oxidizer|{{{oxidiser|}}}}}} / }} {{{fuel|}}}
  }}
<!-- end section for type = solid, liquid, or hybrid parameters -->

<!-- start section for type = solid parameters -->
 | 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|}}} }}
<!-- end section for type = solid parameters -->

<!-- start section for type = liquid parameters -->
 | label30 = Mixture ratio
 | data30 = {{#ifeq:{{{type|}}}|liquid| {{{mixture_ratio|}}} }}

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

 | label32 = Pumps
 | data32 = {{#ifeq:{{{type|}}}|liquid| {{{pumps|}}} }}
<!-- end section for type = liquid parameters -->

 | 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|}}} | &nbsp;&nbsp;&nbsp;&nbsp;at altitude | Thrust (at altitude) }}
 | data52 = {{{thrust_at_altitude|}}}

 | label53 = Thrust (vac.)
 | data53 = {{{thrust(Vac)|}}}

 | label54 = Thrust (SL)
 | 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|''I''<sub>sp</sub>]] (vac.)
 | data63 = {{{specific_impulse_vacuum|}}}

 | label64 = [[Specific impulse|''I''<sub>sp</sub>]] (SL)
 | data64 = {{{specific_impulse_sea_level|}}}

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

 | 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 = Dry weight
 | data84 = {{{dry_weight|}}}
 | 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 = <!--Does not currently exist-->
   | france         = <!--Does not currently exist-->
 }}{{#switch: {{lc:{{{type|}}}}}
   | mono|monopropellant = [[Category:Monopropellant rocket engines]]
   | solid          = <!--Does not currently exist-->
   | liquid         = <!--Does not currently exist-->
   | hybrid         = <!--Does not currently exist-->
 }}
}}<noinclude>
{{Documentation}}
</noinclude>