Template:Infobox rocket engine

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This template uses Lua:

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

Tracking Categories

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 Example NNN 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--> Example NN°	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
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
Spaceflight	astronaut navigation satellite system space agency spaceflight year in spaceflight
Spacecraft	individual space vehicle space shuttle space station module spacecraft class spacecraft instrument docking mechanism
Space program	space program space program by country
Rocketry	launch pad rocket engine launch stage weapon
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