Difference between revisions of "Template:Infobox rocket engine/doc"

From blackwiki
Jump to navigation Jump to search
imported>Anythingcouldhappen
(Added gimbal/TVC to all templates; restart & throttle to all but solid)
(Added mass flow)
 
(5 intermediate revisions by 5 users not shown)
Line 2: Line 2:
 
<!-- PLEASE ADD CATEGORIES AND INTERWIKIS AT THE BOTTOM OF THIS PAGE -->
 
<!-- PLEASE ADD CATEGORIES AND INTERWIKIS AT THE BOTTOM OF THIS PAGE -->
 
{{TOCright}}
 
{{TOCright}}
This template is intended for use on articles about '''[[rocket engine]]s'''. See [[Raptor (rocket engine)|example]] for result.
+
This template is intended for use on articles about '''[[rocket engine]]s''' and '''[[spacecraft propulsion]]'''. See [[SpaceX Raptor|example]] for result.
  
 
== Empty premade templates ==
 
== Empty premade templates ==
Line 40: Line 40:
 
|thrust          =
 
|thrust          =
 
|thrust_at_altitude=
 
|thrust_at_altitude=
|thrust(Vac)    =
+
|thrust(Vac)    =<!--if throttle range >100%, specify corresponding throttle-->
 
|thrust(SL)      =
 
|thrust(SL)      =
|throttle_range  =
+
|throttle_range  =<!--leave blank if no throttle-->
 
|thrust_to_weight=
 
|thrust_to_weight=
 
|chamber_pressure=
 
|chamber_pressure=
Line 49: Line 49:
 
|specific_impulse_sea_level=
 
|specific_impulse_sea_level=
 
|total_impulse  =
 
|total_impulse  =
 +
|mass_flow      =
 
|burn_time      =
 
|burn_time      =
|restarts        =
+
|restarts        =<!--leave blank if not restartable-->
|gimbal          =
+
|gimbal          =<!--gimbal range in °, leave blank if none-->
 
|capacity        =
 
|capacity        =
  
Line 107: Line 108:
 
|specific_impulse_sea_level=
 
|specific_impulse_sea_level=
 
|total_impulse  =
 
|total_impulse  =
 +
|mass_flow      =
 
|burn_time      =
 
|burn_time      =
|gimbal          =
+
|gimbal          =<!--gimbal range in °, or other TVC method, leave blank if none-->
 
|capacity        =
 
|capacity        =
  
Line 153: Line 155:
 
|thrust          =
 
|thrust          =
 
|thrust_at_altitude=
 
|thrust_at_altitude=
|thrust(Vac)    =
+
|thrust(Vac)    =<!--if throttle range >100%, specify corresponding throttle-->
 
|thrust(SL)      =
 
|thrust(SL)      =
|throttle_range  =
+
|throttle_range  =<!--leave blank if no throttle-->
 
|thrust_to_weight=
 
|thrust_to_weight=
 
|chamber_pressure=
 
|chamber_pressure=
Line 162: Line 164:
 
|specific_impulse_sea_level=
 
|specific_impulse_sea_level=
 
|total_impulse  =
 
|total_impulse  =
 +
|mass_flow      =
 
|burn_time      =
 
|burn_time      =
|restarts        =
+
|restarts        =<!--leave blank if not restartable-->
|gimbal          =
+
|gimbal          =<!--gimbal range in °, leave blank if none-->
 
|capacity        =
 
|capacity        =
  
Line 207: Line 210:
 
|thrust          =
 
|thrust          =
 
|thrust_at_altitude=
 
|thrust_at_altitude=
|thrust(Vac)    =
+
|thrust(Vac)    =<!--if throttle range >100%, specify corresponding throttle-->
 
|thrust(SL)      =
 
|thrust(SL)      =
|throttle_range  =
+
|throttle_range  =<!--leave blank if no throttle-->
 
|thrust_to_weight=
 
|thrust_to_weight=
 
|chamber_pressure=
 
|chamber_pressure=
Line 216: Line 219:
 
|specific_impulse_sea_level=
 
|specific_impulse_sea_level=
 
|total_impulse  =
 
|total_impulse  =
 +
|mass_flow      =
 
|burn_time      =
 
|burn_time      =
|restarts        =
+
|restarts        =<!--leave blank if not restartable-->
|gimbal          =
+
|gimbal          =<!--gimbal range in °, leave blank if none-->
 
|capacity        =
 
|capacity        =
  
Line 274: Line 278:
 
==== liquid ====
 
==== liquid ====
 
* '''oxidiser''' / '''fuel'''
 
* '''oxidiser''' / '''fuel'''
* '''mixture_ratio
+
* '''mixture_ratio'''
 
* '''cycle'''
 
* '''cycle'''
 
* '''pumps'''
 
* '''pumps'''
Line 304: Line 308:
 
* '''specific_impulse_sea_level'''
 
* '''specific_impulse_sea_level'''
 
* '''total_impulse'''
 
* '''total_impulse'''
 +
 +
* '''mass_flow'''
  
 
* '''burn_time'''
 
* '''burn_time'''
Line 326: Line 332:
 
{{Spaceflight infoboxes}}
 
{{Spaceflight infoboxes}}
  
<includeonly>
+
<includeonly>{{Sandbox other||
 
<!-- CATEGORIES HERE, THANKS -->
 
<!-- CATEGORIES HERE, THANKS -->
 +
[[Category:Rocketry templates|Rocket engine]]
 
[[Category:Spaceflight infobox templates|Rocket engine]]
 
[[Category:Spaceflight infobox templates|Rocket engine]]
 
[[Category:Technology and applied science infobox templates|Rocket engine]]
 
[[Category:Technology and applied science infobox templates|Rocket engine]]
</includeonly>
+
}}</includeonly>

Latest revision as of 01:33, 11 February 2021

Template:TOCright This template is intended for use on articles about rocket engines and spacecraft propulsion. See example for result.

Empty premade templates

Liquid engines
{{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   =
|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           =
}}
Solid engines
{{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   =
|mass_flow       =
|burn_time       =
|gimbal          =<!--gimbal range in °, or other TVC method, leave blank if none-->
|capacity        =

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

|used_in         =

|references      =
|notes           =
}}
Hybrid engines
{{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   =
|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           =
}}
Monopropellant engines
{{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   =
|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           =
}}

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
  • mass_flow
  • 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

Template:Spaceflight infoboxes