Дидани манбаъи Шаблон:Infobox rocket engine/doc

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This template is intended for use on articles about '''[[rocket engine]]s'''. See [[Raptor (rocket engine)|example]] for result.

== Empty premade templates ==

{| style="background:transparent;"
| width=50% style="vertical-align:top;" |
;Liquid engines
<pre 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
|oxidiser        =
|fuel            =
|mixture_ratio   =
|cycle           =
|pumps           =

|description     =
|combustion_chamber=
|nozzle_ratio    =

|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=
|specific_impulse=
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse   =
|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           =
}}
</pre>
| width=50% style="vertical-align:top;" |
;Solid engines
<pre 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
|oxidiser        =
|fuel            =
|grain           =
|core            =
|casing          =
|nozzle          =

|description     =
|combustion_chamber=
|nozzle_ratio    =

|thrust          =
|thrust_at_altitude=
|thrust(Vac)     =
|thrust(SL)      =
|thrust_to_weight=
|chamber_pressure=
|specific_impulse=
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse   =
|burn_time       =
|gimbal          =<!--gimbal range in °, or other TVC method, leave blank if none-->
|capacity        =

|dimensions      =
|length          =
|diameter        =
|dry_weight      =

|used_in         =

|references      =
|notes           =
}}
</pre>
|-
| width=50% style="vertical-align:top;" |
;Hybrid engines
<pre 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
|oxidiser        =
|fuel            =

|description     =
|combustion_chamber=
|nozzle_ratio    =

|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=
|specific_impulse=
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse   =
|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           =
}}
</pre>
| width=50% style="vertical-align:top;" |
;Monopropellant engines
<pre 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
|fuel            =

|description     =
|combustion_chamber=
|nozzle_ratio    =

|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=
|specific_impulse=
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse   =
|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           =
}}
</pre>
|}

== 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'''
* '''thrust(Vac)'''
* '''thrust(SL)'''
* '''thrust_at_altitude'''
* '''throttle_range'''
* '''thrust_to_weight_ratio'''

* '''specific_impulse'''
* '''specific_impulse_vacuum'''
* '''specific_impulse_sea_level'''
* '''total_impulse'''

* '''burn_time'''
* '''restarts'''
* '''gimbal'''
* '''capacity'''
: tankage

=== Dimensions ===
* '''dimensions''' - use for overall description, otherwise use more specific fields
* '''length'''
* '''diameter'''
* '''dry_weight'''

=== Applications ===
* '''used_in'''

=== References ===
* '''references'''
* '''notes'''

{{Spaceflight infoboxes}}

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[[Category:Spaceflight infobox templates|Rocket engine]]
[[Category:Technology and applied science infobox templates|Rocket engine]]
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