Template:Infobox rocket engine/doc

From The Global Wiki
Jump to navigation Jump to search

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

Script error: No such module "Navbox".


No description.

Template parameters

ParameterDescriptionTypeStatus
namename

no description

Unknownoptional
imageimage

no description

Unknownoptional
image_sizeimage_size

no description

Unknownoptional
imsizeimsize

no description

Unknownoptional
altalt

no description

Unknownoptional
image_altimage_alt

no description

Unknownoptional
captioncaption

no description

Unknownoptional
country_of_origincountry_of_origin

no description

Unknownoptional
datedate

no description

Unknownoptional
first_datefirst_date

no description

Unknownoptional
last_datelast_date

no description

Unknownoptional
designerdesigner

no description

Unknownoptional
manufacturermanufacturer

no description

Unknownoptional
purposepurpose

no description

Unknownoptional
associatedassociated

no description

Unknownoptional
predecessorpredecessor

no description

Unknownoptional
successorsuccessor

no description

Unknownoptional
statusstatus

no description

Unknownoptional
typetype

no description

Unknownoptional
fuelfuel

no description

Unknownoptional
oxidizeroxidizer

no description

Unknownoptional
oxidiseroxidiser

no description

Unknownoptional
graingrain

no description

Unknownoptional
corecore

no description

Unknownoptional
casingcasing

no description

Unknownoptional
nozzlenozzle

no description

Unknownoptional
mixture_ratiomixture_ratio

no description

Unknownoptional
cyclecycle

no description

Unknownoptional
pumpspumps

no description

Unknownoptional
combustion_chambercombustion_chamber

no description

Unknownoptional
nozzle_rationozzle_ratio

no description

Unknownoptional
descriptiondescription

no description

Unknownoptional
thrust(Vac)thrust(Vac)

no description

Unknownoptional
thrust(SL)thrust(SL)

no description

Unknownoptional
thrustthrust

no description

Unknownoptional
thrust_at_altitudethrust_at_altitude

no description

Unknownoptional
thrust_to_weightthrust_to_weight

no description

Unknownoptional
chamber_pressurechamber_pressure

no description

Unknownoptional
specific_impulsespecific_impulse

no description

Unknownoptional
specific_impulse_vacuumspecific_impulse_vacuum

no description

Unknownoptional
specific_impulse_sea_levelspecific_impulse_sea_level

no description

Unknownoptional
total_impulsetotal_impulse

no description

Unknownoptional
burn_timeburn_time

no description

Unknownoptional
capacitycapacity

no description

Unknownoptional
throttle_rangethrottle_range

no description

Unknownoptional
mass_flowmass_flow

no description

Unknownoptional
restartsrestarts

no description

Unknownoptional
gimbalgimbal

no description

Unknownoptional
dimensionsdimensions

no description

Unknownoptional
lengthlength

no description

Unknownoptional
diameterdiameter

no description

Unknownoptional
dry_weightdry_weight

no description

Unknownoptional
used_inused_in

no description

Unknownoptional
embeddedembedded

no description

Unknownoptional
modulemodule

no description

Unknownoptional
referencesreferences

no description

Unknownoptional
notesnotes

no description

Unknownoptional