模板:Infobox rocket engine/doc

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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) = |mass_flow= |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) = |mass_flow= |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) = |mass_flow= |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) = |mass_flow= |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

• 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
• thrust_to_weight_ratio

• specific_impulse
• specific_impulse_vacuum
• specific_impulse_sea_level
• total_impulse

• burn_time

• capacity

tankage

Dimensions

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

Applications

• used_in

References

• references
• notes