ଛାଞ୍ଚ: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.

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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

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

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