Template:Infobox rocket engine

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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      =
|gross           =

|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      =
|gross           =

|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
gross

Applications

used_in

References

references
notes

Tracking Categories

Template Data

TemplateData documentation used by VisualEditor and other tools

See a monthly parameter usage report for Template:Infobox rocket engine in articles based on its TemplateData.

TemplateData for Infobox rocket engine

No description.

Template parameters[Edit template data]

This template has custom formatting.

Parameter		Description	Type	Status
Name	`name`	Name of the rocket engine	String	optional
Image	`image`	Filename for image of the rocket engine, do not include the "File:" or "Image:" prefix	File	optional
Image size	`image_size` `imsize`	Image size in pixels	String	optional
alt	`alt`	no description	Unknown	optional
image_alt	`image_alt`	no description	Unknown	optional
Caption	`caption`	Image caption	String	optional
Country of origin	`country_of_origin`	Country of origin	String	optional
date	`date`	no description	Unknown	optional
First flight date	`first_date`	Date of the first flight, use {{Start date\|YYYY\|MM\|DD\|df=y}} Example{{Start date\|YYYY\|MM\|DD\|df=y}}	String	optional
Last flight date	`last_date`	Date of the last flight, use {{End date\|YYYY\|MM\|DD\|df=y}} Example{{End date\|YYYY\|MM\|DD\|df=y}}	String	optional
Designer	`designer`	Designer of the engine, can be linked	String	optional
Manufacturer	`manufacturer`	Manufacturer of the engine, can be linked, but do not link if the same as the designer	String	optional
purpose	`purpose`	no description	Unknown	optional
Associated launch vehicles	`associated`	List of launch vehicles this rocket engine is associated with	String	optional
Predecessor	`predecessor`	Predecessor rocket engine	String	optional
Successor	`successor`	Successor rocket engine	String	optional
status	`status`	no description	Unknown	optional
Type	`type`	Type of rocket engine, use liquid, solid, hybrid or mono (for monopropellant) Suggested values`liquid` `solid` `hybrid` `mono`	String	required
Fuel	`fuel`	Type of fuel used	String	optional
Oxidizer	`oxidizer` `oxidiser`	Type of oxidizer used	String	optional
grain	`grain`	no description	Unknown	optional
core	`core`	no description	Unknown	optional
casing	`casing`	no description	Unknown	optional
nozzle	`nozzle`	no description	Unknown	optional
mixture_ratio	`mixture_ratio`	no description	Unknown	optional
cycle	`cycle`	no description	Unknown	optional
pumps	`pumps`	no description	Unknown	optional
combustion_chamber	`combustion_chamber`	no description	Unknown	optional
nozzle_ratio	`nozzle_ratio`	no description	Unknown	optional
description	`description`	no description	Unknown	optional
Thrust, vacuum	`thrust(Vac)`	Thrust of the engine, in vacuum, use {{cvt\|VALUEHERE\|kN}} Example{{cvt\|VALUEHERE\|kN}}	String	optional
Thrust, sea level	`thrust(SL)`	Thrust of the engine, at sea level, use {{cvt\|VALUEHERE\|kN}} Example{{cvt\|VALUEHERE\|kN}}	String	optional
Thrust	`thrust`	no description	Unknown	deprecated
thrust_at_altitude	`thrust_at_altitude`	no description	Unknown	optional
thrust_to_weight	`thrust_to_weight`	no description	Unknown	optional
chamber_pressure	`chamber_pressure`	no description	Unknown	optional
Specific impulse	`specific_impulse`	no description	Unknown	deprecated
Specific impulse, vacuum	`specific_impulse_vacuum`	Specific impulse of the engine, in vacuum, use {{cvt\|VALUEHERE\|isp}} Example{{cvt\|VALUEHERE\|isp}}	String	optional
Specific impulse, vacuum	`specific_impulse_sea_level`	Specific impulse of the engine, at sea level, use {{cvt\|VALUEHERE\|isp}} Example{{cvt\|VALUEHERE\|isp}}	Unknown	optional
total_impulse	`total_impulse`	no description	Unknown	optional
Burn time	`burn_time`	The length of time the engine burns normally, in seconds ExampleNNN seconds	String	optional
capacity	`capacity`	no description	Unknown	optional
throttle_range	`throttle_range`	no description	Unknown	optional
mass_flow	`mass_flow`	no description	Unknown	optional
Restarts	`restarts`	How many times the engine can be restarted, leave blank if not restartable	Unknown	optional
Gimbal range	`gimbal`	Gimbal range in °, leave blank if none--> ExampleNN°	String	optional
dimensions	`dimensions`	no description	Unknown	optional
Length	`length`	Length of the engine, in metres, use {{cvt\|VALUE\|m}} Example{{cvt\|VALUE\|m}}	String	optional
Diameter	`diameter`	Diameter of the engine at widest part (typically nozzle tip), in metres, use {{cvt\|VALUE\|m}} Example{{cvt\|VALUE\|m}}	String	optional
Dry weight	`dry_weight`	Mass of unfueled rocket engine in kilograms, use {{cvt\|MASS\|kg}} Example{{cvt\|MASS\|kg}}	String	optional
Gross mass	`gross`	Mass of solid rocket motor with propellant in kilograms, use {{cvt\|MASS\|kg}} Example{{cvt\|MASS\|kg}}	String	optional
used_in	`used_in`	no description	Unknown	optional
embedded	`embedded`	no description	Unknown	optional
module	`module`	no description	Unknown	optional
references	`references`	no description	Unknown	optional
notes	`notes`	no description	Unknown	optional

v t e Spaceflight and rocketry infoboxes
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