Setvadmin: 1 revision imported: Wikipedia Tech Info Boxes

2016-08-21T15:24:01Z

1 revision imported: Wikipedia Tech Info Boxes

Anythingcouldhappen: added reminder to specify throttle level of thrust if needed, other notes

2015-05-31T05:17:04Z

added reminder to specify throttle level of thrust if needed, other notes

New page

{{Documentation subpage}}

{{TOCright}}
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) =
|thrust(SL) =
|throttle_range =
|thrust_to_weight=
|chamber_pressure=
|specific_impulse=
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse =
|burn_time =
|restarts =
|gimbal =
|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 =
|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) =
|thrust(SL) =
|throttle_range =
|thrust_to_weight=
|chamber_pressure=
|specific_impulse=
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse =
|burn_time =
|restarts =
|gimbal =
|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) =
|thrust(SL) =
|throttle_range =
|thrust_to_weight=
|chamber_pressure=
|specific_impulse=
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse =
|burn_time =
|restarts =
|gimbal =
|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}}

<includeonly>

[[Category:Spaceflight infobox templates|Rocket engine]]
[[Category:Technology and applied science infobox templates|Rocket engine]]
</includeonly>

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Setvadmin: 1 revision imported: Wikipedia Tech Info Boxes

Anythingcouldhappen: added reminder to specify throttle level of thrust if needed, other notes