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Template:Rocket engines

From Wikipedia, the free encyclopedia
Liquid
fuel
Cryogenic
Hydrolox
(LH2 /LOX)
Methalox
(CH4 /LOX)
Semi-
cryogenic
Kerolox
(RP-1 /LOX)
Storable
Hypergolic (Aerozine,
UH 25,MMH, orUDMH
/N2O4,MON, orHNO3)
Other
Solid
fuel
  • * Different versions of the engine use different propellant combinations
  • Engines initalics are/were under development
Template documentation[view] [edit] [history] [purge]

Scope

[edit]

This template is used exclusively forflown rocket engines used onorbitallaunch vehicles. The decision is on the intent of the vehicle, a suborbital mission of an orbital launch vehicle sill counts.Sub-orbital launch vehiclesper se are excluded, anything atmospheric in not part of this. Pure orbital spacecraft, i.e. the payload of a launch vehicle, does not count.

Acceptable

NOT acceptable:

Acceptability

[edit]

This template is for rocket engines that have flown or are expected to fly in the near term. Engines not yet flown should be inItalics. The criteria for acceptability of unflown rocket engines are:

Option A

  • The engine has an article of at leastStart class.
  • The engine has been test fired, at least at the flight component or sub-scale level.
  • The intent is for the rocket to be used in an orbital launch vehicle in the next five years.

Examples:SCE-200 orRaptor (rocket engine) as of 2016.

Option B

  • The engine has an article of at leastStart class.
  • The engine has been test fired at the flight model level (i.e. as intended to fly).
  • The engine was intended for use in an orbital launch vehicle but it was never actually used.

Example:RD-270 as of 2016, butNOT theIPD which lacked a thrust chamber and was not intended to fly.

Categorization

[edit]

Some guidance for placing rocket engines on the template:

  • Country: the country that counts is the designer's country. So, for example, theRD-120 was designed in Russia byNPO Energomash, and built in Ukraine byYuzhmash, but counts as Russian. For countries that have disappeared, we display their mainsuccessor state, e.g. Russia for the Soviet Union.
  • Propellant: Care should be used not to increase too much the number of propellants. Exotic propellants like theRD-119 or the Nth variation ofHydrazine should all be clumped together.
  • Rocket families: Only different number variations should be included, and should be grouped bycomma separation or, in more than two sequential numbers, through the use of theto word. For example theRD-0210 is presented asRD-0202 to RD-0206, RD-0208 to 0213, but the wholeMerlin 1 family goes in one entry, notA,B,C,D,D Vacuum distinction.
  • Ordering: within each propellant and country the engines order should bestrictly alphabetical.

Options

Place{{Rocket engines}} at the end of an article, but above any categories.

This template'sinitial visibility currently defaults toautocollapse, meaning that if there is another collapsible item on the page (anavbox, sidebar, ortable with the collapsible attribute), it is hidden apart from its title bar; if not, it is fully visible.

To change this template's initial visibility, the|state=parameter may be used:

  • {{Rocket engines|state=collapsed}} will show the template collapsed, i.e. hidden apart from its title bar.
  • {{Rocket engines|state=expanded}} will show the template expanded, i.e. fully visible.
  • {{Rocket engines|state=autocollapse}} will show the template autocollapsed, i.e. if there is another collapsible item on the page (anavbox, sidebar, ortable with the collapsible attribute), it is hidden apart from its title bar, but if not, it is fully visible.
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The abovedocumentation istranscluded fromTemplate:Rocket engines/doc.(edit |history)
Editors can experiment in this template's sandbox(create |mirror) and testcases(create) pages.
Add categories to the/doc subpage.Subpages of this template.
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