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Template:Infobox rocket engine/doc

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This is an old revision of this page, as edited by Leafnode (talk | contribs) at 08:07, 12 August 2011 (+interwiki). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

An infobox template for describing rocket engines.

Yes, there are other templates around for rockets. However they're all either vehicles {{Infobox Rocket}} or stages {{Infobox Rocket stage}}. I haven't yet found one for engines.

This template is very new, so likely to change imminently. If you wish to edit it, please use Template talk:Infobox rocket engine/doc first.
Andy Dingley (talk) 18:51, 17 April 2008 (UTC)

Parameters

Image

  • image (optional)
  • caption (optional)
  • imsize (optional)

Origins

  • name (required)
  • country of origin (optional)
  • date (optional)
  • first flight (optional)
  • last flight (optional)
  • designer (optional)
  • manufacturer (optional)
  • purpose (optional)
"booster", "apogee kick" etc.
  • predecessor (optional)
  • successor (optional)
  • associated (optional)
  • status (optional)

Type

  • type (required)
    • solid
    • liquid
    • hybrid
    • mono / monopropellant
    • other - free-text

Solids

  • grain (optional)
Use for simple overall description, otherwise use the more-specific parameters below
  • oxidiser / fuel (optional)
  • core (optional)
  • casing (optional)
  • nozzle (optional)

liquid

  • fuel (required)
  • oxidizer / oxidiser (required)
  • cycle (optional)
  • pumps (optional)
free text, describe the fuel system
  • combustion_chamber (optional)
  • nozzle_ratio (optional)

hybrid

  • fuel (required)
  • oxidizer / oxidiser (required)


monopropellant

  • fuel (required)

others

Just use the description

Description

  • description (optional)

Performance

  • thrust (optional)
  • thrust(Vac) (optional)
  • thrust(SL) (optional)
  • thrust_at_altitude (optional)
  • thrust_to_weight_ratio (optional)
  • specific_impulse (optional)
  • specific_impulse_vacuum (optional)
  • specific_impulse_sea_level (optional)
  • total_impulse (optional)
  • burn_time (optional)
  • capacity
tankage

Dimensions

  • dimensions (optional)
use for overall descrioption, otherwise use the more specifics
  • length (optional)
  • diameter (optional)
  • dry_weight (optional)

Applications

  • used_in

Styling

  • class, style
CSS parameters, applied to the overall infobox table.

References

  • references (optional)

Others

Other parameters (not yet implemented) could be:


Categorization

Categorizes into Category:Rocket engines and also potentially some combination of Category:Solid-fuel rocket motors, Category:British rocket engines etc.