మూస:Infobox rocket engine
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This template is intended for use on articles about rocket engines. See example for result.
Empty premade templates[మార్చు]
{{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) = |thrust(SL) = |thrust_to_weight= |chamber_pressure= |specific_impulse= |specific_impulse_vacuum= |specific_impulse_sea_level= |total_impulse = |burn_time = |capacity = |dimensions = |length = |diameter = |dry_weight = |used_in = |references = |notes = }} |
{{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 = |burn_time = |capacity = |dimensions = |length = |diameter = |dry_weight = |used_in = |references = |notes = }} |
{{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) = |thrust(SL) = |thrust_to_weight= |chamber_pressure= |specific_impulse= |specific_impulse_vacuum= |specific_impulse_sea_level= |total_impulse = |burn_time = |capacity = |dimensions = |length = |diameter = |dry_weight = |used_in = |references = |notes = }} |
{{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) = |thrust(SL) = |thrust_to_weight= |chamber_pressure= |specific_impulse= |specific_impulse_vacuum= |specific_impulse_sea_level= |total_impulse = |burn_time = |capacity = |dimensions = |length = |diameter = |dry_weight = |used_in = |references = |notes = }} |
Parameters[మార్చు]
- name
Image[మార్చు]
- image
- caption
- imsize
Origins[మార్చు]
- country of origin
- date
- first flight
- last flight
- designer
- manufacturer
- purpose - "booster", "apogee kick", etc.
- predecessor
- successor
- associated
- status
Type[మార్చు]
- type
- solid
- liquid
- hybrid
- mono / monopropellant
Solids[మార్చు]
- oxidiser / fuel
- grain
- core
- casing
- nozzle
liquid[మార్చు]
- oxidiser / fuel
- mixture_ratio
- cycle
- pumps
hybrid[మార్చు]
- oxidiser / fuel
monopropellant[మార్చు]
- fuel
others[మార్చు]
Just use the "type" and "description" fields.
Configuration[మార్చు]
- description
- combustion_chamber
- nozzle_ratio
Performance[మార్చు]
- thrust
- thrust(Vac)
- thrust(SL)
- thrust_at_altitude
- thrust_to_weight_ratio
- specific_impulse
- specific_impulse_vacuum
- specific_impulse_sea_level
- total_impulse
- burn_time
- capacity
- tankage
Dimensions[మార్చు]
- dimensions - use for overall description, otherwise use more specific fields
- length
- diameter
- dry_weight
Applications[మార్చు]
- used_in
References[మార్చు]
- references
- notes