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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[edit]

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[edit]

name

Image[edit]

image
caption
imsize

Origins[edit]

country of origin
date
first flight
last flight

designer
manufacturer

purpose - "booster", "apogee kick", etc.

predecessor
successor
associated
status

Type[edit]

type
- solid
- liquid
- hybrid
- mono / monopropellant

Solids[edit]

oxidiser / fuel
grain
core
casing
nozzle

liquid[edit]

oxidiser / fuel
mixture_ratio
cycle
pumps

hybrid[edit]

oxidiser / fuel

monopropellant[edit]

fuel

others[edit]

Just use the "type" and "description" fields.

Configuration[edit]

description
combustion_chamber
nozzle_ratio

Performance[edit]

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[edit]

dimensions - use for overall description, otherwise use more specific fields
length
diameter
dry_weight

Applications[edit]

used_in

References[edit]

references
notes

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 (American English) space programme (non-American English) space program by country
Rocketry	launch pad rocket engine launch stage weapon
See also Category:Rocketry templates Category:Spaceflight infobox templates ((Spaceflight navboxes)) WikiProject Rocketry WikiProject Spaceflight

No description.

Template parameters[Edit template data]
Parameter		Description	Type	Status
name	`name`	no description	Unknown	optional
image	`image`	no description	Unknown	optional
image_size	`image_size`	no description	Unknown	optional
imsize	`imsize`	no description	Unknown	optional
alt	`alt`	no description	Unknown	optional
image_alt	`image_alt`	no description	Unknown	optional
caption	`caption`	no description	Unknown	optional
country_of_origin	`country_of_origin`	no description	Unknown	optional
date	`date`	no description	Unknown	optional
first_date	`first_date`	no description	Unknown	optional
last_date	`last_date`	no description	Unknown	optional
designer	`designer`	no description	Unknown	optional
manufacturer	`manufacturer`	no description	Unknown	optional
purpose	`purpose`	no description	Unknown	optional
associated	`associated`	no description	Unknown	optional
predecessor	`predecessor`	no description	Unknown	optional
successor	`successor`	no description	Unknown	optional
status	`status`	no description	Unknown	optional
type	`type`	no description	Unknown	optional
fuel	`fuel`	no description	Unknown	optional
oxidizer	`oxidizer`	no description	Unknown	optional
oxidiser	`oxidiser`	no description	Unknown	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(Vac)	`thrust(Vac)`	no description	Unknown	optional
thrust(SL)	`thrust(SL)`	no description	Unknown	optional
thrust	`thrust`	no description	Unknown	optional
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	optional
specific_impulse_vacuum	`specific_impulse_vacuum`	no description	Unknown	optional
specific_impulse_sea_level	`specific_impulse_sea_level`	no description	Unknown	optional
total_impulse	`total_impulse`	no description	Unknown	optional
burn_time	`burn_time`	no description	Unknown	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`	no description	Unknown	optional
gimbal	`gimbal`	no description	Unknown	optional
dimensions	`dimensions`	no description	Unknown	optional
length	`length`	no description	Unknown	optional
diameter	`diameter`	no description	Unknown	optional
dry_weight	`dry_weight`	no description	Unknown	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

The above documentation is transcluded from Template:Infobox rocket engine/doc.
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