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Template:Rocket engines

{{Navbox

|name = Rocket engines

|title = Rocket engines and solid motors for orbital launch vehicles

|bodyclass = hlist

|state = {{{state|autocollapse}}}

|image = Image:RS-68 rocket engine test.jpg

|group1 = Liquid
fuel

|list1 = {{Navbox|subgroup

|group1 = Cryogenic

|list1 = {{Navbox|subgroup

|group1 = Hydrolox
(LH2 / LOX)

|list1 =

|group2 = Methalox
(CH4 / LOX)

|list2 =

}}

|group2 = Semi-
cryogenic

|list2 = {{navbox|subgroup

|group1 = Kerolox
(RP-1 / LOX)

|list1 =

}}

|group3 = Storable

|list3 = {{navbox|subgroup

|group1 = Hypergolic (Aerozine,
UH 25, MMH, or UDMH
/ N2O4, MON, or HNO3)

|list1 =

}}

|group4 = Other

|list4 =

}}

|group2 = Solid
fuel

|list2 =

|above =

|below =

  • * Different versions of the engine use different propellant combinations
  • Engines in italics are under development

}}

{{documentation}}