Template:Infobox rocket engine/doc
![]() | This is a documentation subpage for Template:Infobox rocket engine. It may contain usage information, categories and other content that is not part of the original template page. |
![]() | 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
<syntaxhighlight lang="wikitext" style="overflow:auto;">
</syntaxhighlight> |
<syntaxhighlight lang="wikitext" style="overflow:auto;">
</syntaxhighlight> | ||||
<syntaxhighlight lang="wikitext" style="overflow:auto;">
</syntaxhighlight> |
<syntaxhighlight lang="wikitext" style="overflow:auto;">
</syntaxhighlight> |
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
- Category:Pages using infobox rocket engine with unknown parameters (1)
- Category:Rocket engines of the United Kingdom (9)
- Category:Rocket engines of the Soviet Union (47)
- Category:Monopropellant rocket engines (3)
See Also