Template:Infobox rocket engine/doc: Difference between revisions

Content deleted Content added
mv cat
Add blank fields, bit of cleanup of redundant stuff.
Line 2:
<!-- PLEASE ADD CATEGORIES AND INTERWIKIS AT THE BOTTOM OF THIS PAGE -->
{{TOCright}}
An infoboxThis template is intended for describinguse on articles about '''[[rocket enginesengine]]s'''.
 
== 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% valign=top |
<br>[[User:Andy Dingley|Andy Dingley]] ([[User talk:Andy Dingley|talk]]) 18:51, 17 April 2008 (UTC)
;Liquid engines
<pre style="overflow:auto;">
{{Infobox rocket engine
|name =
|image =
|imsize =
|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) =
|thrust_to_weight=
|chamber_pressure=
|specific_impulse=
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse =
|burn_time =
|capacity =
 
|dimensions =
|length =
|diameter =
|dry_weight =
 
|used_in =
 
|references =
|notes =
}}
</pre>
| width=50% valign=top |
;Solid engines
<pre style="overflow:auto;">
{{Infobox rocket engine
|name =
|image =
|imsize =
|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 =
|capacity =
 
|dimensions =
|length =
|diameter =
|dry_weight =
 
|used_in =
 
|references =
|notes =
}}
</pre>
|-
| width=50% valign=top |
;Hybrid engines
<pre style="overflow:auto;">
{{Infobox rocket engine
|name =
|image =
|imsize =
|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) =
|thrust_to_weight=
|chamber_pressure=
|specific_impulse=
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse =
|burn_time =
|capacity =
 
|dimensions =
|length =
|diameter =
|dry_weight =
 
|used_in =
 
|references =
|notes =
}}
</pre>
| width=50% valign=top |
;Monopropellant engines
<pre style="overflow:auto;">
{{Infobox rocket engine
|name =
|image =
|imsize =
|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) =
|thrust_to_weight=
|chamber_pressure=
|specific_impulse=
|specific_impulse_vacuum=
|specific_impulse_sea_level=
|total_impulse =
|burn_time =
|capacity =
 
|dimensions =
|length =
|diameter =
|dry_weight =
 
|used_in =
 
|references =
|notes =
}}
</pre>
|}
 
== Parameters ==
* '''name'''
 
=== Image ===
* '''image''' (optional)
* '''caption''' (optional)
* '''imsize''' (optional)
 
=== Origins ===
* '''namecountry of origin''' (required)
* '''date'''
* '''first flight'''
* '''last flight'''
 
* '''country of origindesigner''' (optional)
* '''datemanufacturer''' (optional)
* '''first flight''' (optional)
* '''last flight''' (optional)
 
* '''purpose''' - "booster", "apogee kick", etc.
* '''designer''' (optional)
* '''manufacturer''' (optional)
 
* '''purposepredecessor''' (optional)
* '''successor'''
: "booster", "apogee kick" etc.
* '''associated'''
 
* '''predecessorstatus''' (optional)
* '''successor''' (optional)
* '''associated''' (optional)
* '''status''' (optional)
 
=== Type ===
* '''type''' (required)
** solid
** liquid
** hybrid
** mono / monopropellant
** ''other'' - free-text
 
==== Solids ====
* '''grainoxidiser''' (optional)/ '''fuel'''
* '''grain'''
: Use for simple overall description, otherwise use the more-specific parameters below
* '''core'''
* '''oxidiser''' / '''fuel''' (optional)
* '''corecasing''' (optional)
* '''casingnozzle''' (optional)
* '''nozzle''' (optional)
 
==== liquid ====
* '''fueloxidiser''' (required)/ '''fuel'''
* '''mixture_ratio
* '''cycle'''
* '''pumps'''
 
==== hybrid ====
* '''oxidizer''' / '''oxidiser''' (required)
* '''oxidiser''' / '''fuel'''
 
==== monopropellant ====
* '''cycle''' (optional)
* '''pumpsfuel''' (optional)
: free text, describe the fuel system
 
==== others ====
* '''combustion_chamber''' (optional)
Just use the "type" and "description" fields.
* '''nozzle_ratio''' (optional)
 
====hybrid= Configuration ===
* '''fueldescription''' (required)
* '''combustion_chamber'''
 
* '''nozzle_ratio'''
* '''oxidizer''' / '''oxidiser''' (required)
 
====monopropellant====
* '''fuel''' (required)
 
====others====
Just use the description
 
===Description===
* '''description''' (optional)
 
=== Performance ===
* '''thrust''' (optional)
* '''thrust(Vac)''' (optional)
* '''thrust(SL)''' (optional)
* '''thrust_at_altitude''' (optional)
* '''thrust_to_weight_ratio''' (optional)
 
* '''specific_impulse''' (optional)
* '''specific_impulse_vacuum''' (optional)
* '''specific_impulse_sea_level''' (optional)
* '''total_impulse''' (optional)
 
* '''burn_time''' (optional)
 
* '''capacity'''
Line 94 ⟶ 300:
 
=== Dimensions ===
* '''dimensions''' (optional)- use for overall description, otherwise use more specific fields
* '''length'''
: use for overall descrioption, otherwise use the more specifics
* '''lengthdiameter''' (optional)
* '''diameterdry_weight''' (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:
 
== Categorization ==
Categorizes into [[:Category:Rocket engines]] and also potentially some combination of [[:Category:Solid-fuel rocket motors]], [[:Category:British rocket engines]] etc.
 
{{Spaceflight infoboxes}}