Şablon:Infobox rocket engine

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This template is intended for use on articles about rocket engines.

Empty premade templates[bıvurne | çımey bıvurne]

Liquid engines
{{Infobox rocket engine
|name            =
|image           =
|imsize          =
|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           =
}}
Solid engines
{{Infobox rocket engine
|name            =
|image           =
|imsize          =
|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           =
}}
Hybrid engines
{{Infobox rocket engine
|name            =
|image           =
|imsize          =
|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           =
}}
Monopropellant engines
{{Infobox rocket engine
|name            =
|image           =
|imsize          =
|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[bıvurne | çımey bıvurne]

  • name

Image[bıvurne | çımey bıvurne]

  • image
  • caption
  • imsize

Origins[bıvurne | çımey bıvurne]

  • country of origin
  • date
  • first flight
  • last flight
  • designer
  • manufacturer
  • purpose - "booster", "apogee kick", etc.
  • predecessor
  • successor
  • associated
  • status

Type[bıvurne | çımey bıvurne]

  • type
    • solid
    • liquid
    • hybrid
    • mono / monopropellant

Solids[bıvurne | çımey bıvurne]

  • oxidiser / fuel
  • grain
  • core
  • casing
  • nozzle

liquid[bıvurne | çımey bıvurne]

  • oxidiser / fuel
  • mixture_ratio
  • cycle
  • pumps

hybrid[bıvurne | çımey bıvurne]

  • oxidiser / fuel

monopropellant[bıvurne | çımey bıvurne]

  • fuel

others[bıvurne | çımey bıvurne]

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

Configuration[bıvurne | çımey bıvurne]

  • description
  • combustion_chamber
  • nozzle_ratio

Performance[bıvurne | çımey bıvurne]

  • 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[bıvurne | çımey bıvurne]

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

Applications[bıvurne | çımey bıvurne]

  • used_in

References[bıvurne | çımey bıvurne]

  • references
  • notes