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{{Documentation subpage}}
<!-- Please place categories where indicated at the bottom of this page and interwikis at Wikidata (see [[Wikipedia:Wikidata]]) -->
{{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.
== Empty premade templates ==
{| style="background:transparent;"
| width=50%
;Liquid engines
<
{{Infobox rocket engine
|name =
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|thrust =
|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=
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|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 =
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|notes =
}}
</syntaxhighlight>
| width=50%
;Solid engines
<
{{Infobox rocket engine
|name =
|image =
|
|caption =
|country_of_origin=
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|specific_impulse_sea_level=
|total_impulse =
|mass_flow =
|burn_time =
|gimbal =<!--gimbal range in °, or other TVC method, leave blank if none-->
|capacity =
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|diameter =
|dry_weight =
|gross =
|used_in =
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|notes =
}}
</syntaxhighlight>
|-
| width=50%
;Hybrid engines
<
{{Infobox rocket engine
|name =
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|thrust =
|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=
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|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 =
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|diameter =
|dry_weight =
|gross =
|used_in =
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|notes =
}}
</syntaxhighlight>
| width=50%
;Monopropellant engines
<
{{Infobox rocket engine
|name =
|image =
|
|caption =
|country_of_origin=
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|thrust =
|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=
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|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 =
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|notes =
}}
</syntaxhighlight>
|}
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==== liquid ====
* '''oxidiser''' / '''fuel'''
* '''mixture_ratio'''
* '''cycle'''
* '''pumps'''
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* '''thrust(SL)'''
* '''thrust_at_altitude'''
* '''throttle_range'''
* '''thrust_to_weight_ratio'''
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* '''total_impulse'''
* '''
* '''burn_time'''
* '''restarts'''
* '''gimbal'''
* '''capacity'''
: tankage
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* '''diameter'''
* '''dry_weight'''
* '''gross'''
=== Applications ===
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* '''notes'''
=== Tracking Categories ===
* {{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 ==
{{Spaceflight infoboxes}}
<includeonly>{{Sandbox other||
<!-- Categories below this line, please; interwikis at Wikidata -->
[[Category:Rocketry templates|Rocket engine]]
[[Category:Spaceflight infobox templates|Rocket engine]]
[[Category:Technology and applied science infobox templates|Rocket engine]]
[[Category:Infobox templates with module parameter]]
}}</includeonly>
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