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{{Documentation subpage}}
<!-- Please place categories where indicated at the bottom of this page and interwikis at Wikidata (see [[Wikipedia:Wikidata]]) -->
<!-- PLEASE ADD CATEGORIES AND INTERWIKIS AT THE BOTTOM OF THIS PAGE -->
{{Lua|Module:Infobox|Module:InfoboxImage|Module:Check for unknown parameters}}
{{TOCright}}
This template is intended for use on articles about '''[[rocket engine]]s''' and '''[[spacecraft propulsion]]'''. See [[SpaceX Raptor|example]] for result.
An infobox template for describing rocket engines.
 
== Empty premade templates ==
Yes, there are other templates around for rockets. However they're all either vehicles {{tl|Infobox Rocket}} or stages {{tl|Infobox Rocket stage}}. I haven't yet found one for engines.
 
{| style="background:transparent;"
This template is very new, so likely to change imminently. If you wish to edit it, please use [[{{TALKPAGENAME}}]] first.
| width=50% style="vertical-align:top;" |
<br>[[User:Andy Dingley|Andy Dingley]] ([[User talk:Andy Dingley|talk]]) 18:51, 17 April 2008 (UTC)
;Liquid engines
<syntaxhighlight lang="wikitext" style="overflow:auto;">
{{Infobox rocket engine
|name =
|image =
|image_size =
|caption =
|country_of_origin=
|date =
|first_date =
|last_date =
|designer =
|manufacturer =
|purpose =
|associated =
|predecessor =
|successor =
|status =
 
|type =liquid
== Parameters ==
|oxidiser =
|fuel =
|mixture_ratio =
|cycle =
|pumps =
 
|description =
=== Image ===
|combustion_chamber=
|nozzle_ratio =
 
|thrust =
* '''image''' (optional)
|thrust_at_altitude=
* '''caption''' (optional)
|thrust(Vac) =<!--if throttle range >100%, specify corresponding throttle-->
* '''imsize''' (optional)
|thrust(SL) =
|throttle_range =<!--leave blank if no throttle-->
|thrust_to_weight=
|chamber_pressure=
|specific_impulse=
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse =
|mass_flow =
|burn_time =
|restarts =<!--leave blank if not restartable-->
|gimbal =<!--gimbal range in °, leave blank if none-->
|capacity =
 
|dimensions =
=== Origins ===
|length =
* '''name''' (required)
|diameter =
|dry_weight =
 
|used_in =
* '''country of origin''' (optional)
* '''date'''(optional)
 
|references =
* '''designer''' (optional)
|notes =
* '''manufacturer''' (optional)
}}
</syntaxhighlight>
| width=50% style="vertical-align:top;" |
;Solid engines
<syntaxhighlight lang="wikitext" style="overflow:auto;">
{{Infobox rocket engine
|name =
|image =
|image_size =
|caption =
|country_of_origin=
|date =
|first_date =
|last_date =
|designer =
|manufacturer =
|purpose =
|associated =
|predecessor =
|successor =
|status =
 
|type =solid
* '''purpose''' (optional)
|oxidiser =
: "booster", "apogee kick" etc.
|fuel =
|grain =
|core =
|casing =
|nozzle =
 
|description =
* '''predecessor''' (optional)
|combustion_chamber=
* '''successor''' (optional)
|nozzle_ratio =
* '''status''' (optional)
 
|thrust =
=== Type ===
|thrust_at_altitude=
* '''type''' (required)
|thrust(Vac) =
** solid
|thrust(SL) =
** liquid
|thrust_to_weight=
** hybrid
|chamber_pressure=
** mono / monopropellant
|specific_impulse=
** ''other'' - free-text
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse =
|mass_flow =
|burn_time =
|gimbal =<!--gimbal range in °, or other TVC method, leave blank if none-->
|capacity =
 
|dimensions =
====Solids====
|length =
* '''grain''' (optional)
|diameter =
: Use for simple overall description, otherwise use the more-specific parameters below
|dry_weight =
* '''oxidiser''' / '''fuel''' (optional)
|gross =
* '''core''' (optional)
* '''casing''' (optional)
* '''nozzle''' (optional)
 
|used_in =
====liquid====
* '''fuel''' (required)
 
|references =
* '''oxidizer''' / '''oxidiser''' (required)
|notes =
}}
</syntaxhighlight>
|-
| width=50% style="vertical-align:top;" |
;Hybrid engines
<syntaxhighlight lang="wikitext" style="overflow:auto;">
{{Infobox rocket engine
|name =
|image =
|image_size =
|caption =
|country_of_origin=
|date =
|first_date =
|last_date =
|designer =
|manufacturer =
|purpose =
|associated =
|predecessor =
|successor =
|status =
 
|type =hybrid
* '''cycle''' (optional)
|oxidiser =
* '''pumps''' (optional)
|fuel =
: fre text, describe the fuel system
 
|description =
* '''combustion_chamber''' (optional)
|combustion_chamber=
|nozzle_ratio =
 
|thrust =
====hybrid====
|thrust_at_altitude=
* '''fuel''' (required)
|thrust(Vac) =<!--if throttle range >100%, specify corresponding throttle-->
|thrust(SL) =
|throttle_range =<!--leave blank if no throttle-->
|thrust_to_weight=
|chamber_pressure=
|specific_impulse=
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse =
|mass_flow =
|burn_time =
|restarts =<!--leave blank if not restartable-->
|gimbal =<!--gimbal range in °, leave blank if none-->
|capacity =
 
|dimensions =
* '''oxidizer''' / '''oxidiser''' (required)
|length =
|diameter =
|dry_weight =
|gross =
 
|used_in =
 
|references =
====monopropellant====
|notes =
* '''fuel''' (required)
}}
</syntaxhighlight>
| width=50% style="vertical-align:top;" |
;Monopropellant engines
<syntaxhighlight lang="wikitext" style="overflow:auto;">
{{Infobox rocket engine
|name =
|image =
|image_size =
|caption =
|country_of_origin=
|date =
|first_date =
|last_date =
|designer =
|manufacturer =
|purpose =
|associated =
|predecessor =
|successor =
|status =
 
|type =mono
====others====
|fuel =
Just use the description
 
|description =
===Description===
|combustion_chamber=
|nozzle_ratio =
 
|thrust =
* '''description''' (optional)
|thrust_at_altitude=
|thrust(Vac) =<!--if throttle range >100%, specify corresponding throttle-->
|thrust(SL) =
|throttle_range =<!--leave blank if no throttle-->
|thrust_to_weight=
|chamber_pressure=
|specific_impulse=
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse =
|mass_flow =
|burn_time =
|restarts =<!--leave blank if not restartable-->
|gimbal =<!--gimbal range in °, leave blank if none-->
|capacity =
 
|dimensions =
|length =
|diameter =
|dry_weight =
 
|used_in =
 
|references =
|notes =
}}
</syntaxhighlight>
|}
 
== Parameters ==
* '''name'''
 
=== Image ===
* '''image'''
* '''caption'''
* '''imsize'''
 
=== Origins ===
* '''country of origin'''
* '''date'''
* '''first flight'''
* '''last flight'''
 
* '''designer'''
* '''manufacturer'''
 
* '''purpose''' - "booster", "apogee kick", etc.
 
* '''predecessor'''
* '''successor'''
* '''associated'''
* '''status'''
 
=== Type ===
* '''type'''
** solid
** liquid
** hybrid
** mono / monopropellant
 
==== Solids ====
* '''oxidiser''' / '''fuel'''
* '''grain'''
* '''core'''
* '''casing'''
* '''nozzle'''
 
==== liquid ====
* '''oxidiser''' / '''fuel'''
* '''mixture_ratio'''
* '''cycle'''
* '''pumps'''
 
==== hybrid ====
* '''oxidiser''' / '''fuel'''
 
==== monopropellant ====
* '''fuel'''
 
==== others ====
Just use the "type" and "description" fields.
 
=== Configuration ===
* '''description'''
* '''combustion_chamber'''
* '''nozzle_ratio'''
 
=== Performance ===
* '''thrust''' (optional)
* '''thrust(Vac)''' (optional)
* '''thrust(SL)''' (optional)
* '''thrust_at_altitude''' (optional)
* '''throttle_range'''
* '''thrust_to_weight_ratio''' (optional)
* '''thrust_to_weight_ratio'''
 
* '''specific_impulse''' (optional)
* '''specific_impulse_vacuum''' (optional)
* '''specific_impulse_sea_level''' (optional)
* '''total_impulse''' (optional)
 
* '''burn_timemass_flow''' (optional)
 
* '''burn_time'''
* '''restarts'''
* '''gimbal'''
* '''capacity'''
: tankage
 
=== Dimensions ===
* '''dimensions''' - use for overall description, otherwise use more specific fields
 
* '''dimensionslength''' (optional)
* '''diameter'''
: use for overall descrioption, otherwise use the more specifics
* '''lengthdry_weight''' (optional)
* '''diametergross''' (optional)
* '''dry_weight''' (optional)
 
=== Applications ===
* '''used_in'''
 
=== StylingReferences ===
* '''class''', '''style references'''
* '''notes'''
: CSS parameters, applied to the overall infobox table.
 
=== References===
* '''references''' (optional)
 
=== Others ===
Other parameters (not yet implemented) could be:
 
 
=== Tracking Categories ===
== Categorization ==
* {{Category link with count|Pages using infobox rocket engine with unknown parameters}}
* {{Category link with count|Rocket engines of the United Kingdom}}
* {{Category link with count|Category:Rocket engines of the Soviet Union}}
* {{Category link with count|Category:Monopropellant rocket engines}}
 
== See Also ==
Categorizes into [[:Category:Rocket engines]] and also potentially some combination of [[:Category:Solid-fuel rocket motors]], [[:Category:British rocket engines]] etc.
{{Spaceflight infoboxes}}
<includeonly>
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<includeonly>{{Sandbox other||
<!-- Categories below this line, please; interwikis at Wikidata -->
 
[[Category:Rocketry templates|Rocket engine]]
</includeonly>
[[Category:Spaceflight infobox templates|Rocket engine]]
[[Category:Technology and applied science infobox templates|Rocket engine]]
[[Category:Infobox templates with module parameter]]
}}</includeonly>
Retrieved from "https://en.wikipedia.org/wiki/Template:Infobox_rocket_engine/doc"