Templat:Mesin roket: Perbedaan antara revisi

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Ssafasad (bicara | kontrib)
from en:Template:Rocket Engines 5 October 2015, at 05:02.
 
Ssafasad (bicara | kontrib)
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Baris 4:
|name = Rocket Engines
|image = [[Image:RS-68 rocket engine test.jpg|120px|alt=|link=]]
|group1 = [[Liquid-propellantRoket rocketpropelan cair|Liquid fuel]]
|list1 = {{Navbox subgroup
|group1 = [[CryogenicKriogenik fuel(bahan bakar)|CryogenicKriogenik]] <br/><br/> ([[LiquidHidrogen hydrogencair|LH<sub>2</sub>]]/[[LiquidOksigen oxygencair|LOX]])
 
|list1 = {{Navbox subgroup|groupstyle=width:8em;|liststyle = width:auto;
|group1 = US
|list1 =
* [[Rocketdyne J-2 (rocket engine)|J-2]]
* [[RL10]]
* [[RS-68]]
* [[SpaceMesin ShuttleUtama mainPesawat engineUlang alik|RS-25 (SSME)]]
|group2 = EU
|list2 =
Baris 21:
|group3 = Russia
|list3 =
* [[RD-0120 (rocketmesin engineroket)|RD-0120]]
* [[:en:KVD-1|KVD-1 (RD-56)]]
|group4 = Japan
|list4 =
Baris 37:
|group2 =
|list2 =
|group3 = Semi-cryogenic <br/><br/> ([[RP-1]]/[[LiquidOksigen oxygencair|LOX]])
|list3 = {{Navbox subgroup|groupstyle=width:9em;|liststyle = width:auto;
|group1 = US
|list1 =
* [[F-1 (rocketmesin engineroket)|F-1]]
* [[H-1 (rocketmesin engineroket)|H-1]]
* [[Kestrel (rocketmesin engineroket)|Kestrel]]
* [[:en:PGM-17_Thor#Specifications (PGM-17A)|LR-79]]
* [[:en:SM-65 Atlas#Specifications (Atlas ICBM)|LR-89]]
* [[:en:SM-65 Atlas#Specifications (Atlas ICBM)|LR-105]]
* [[Merlin (rocketmesin engine familyroket)|Merlin 1]]
* [[RS-27]]
* [[RS-27A]]
* [[:en:Atlas II|RS-58]]
* [[XLR50]]
|group2 = EU
Baris 59:
* [[NK-33]]
* [[RD-0105]]
* [[RD-107|RD-0107]]
* [[RD-0108]]
* [[RD-0109]]
Baris 69:
* [[RD-117]]
* [[RD-120]]
* [[RD-170 (rocketmesin engineroket)|RD-170]]
* [[RD-180]]
* [[RD-191]]
* [[RD-58]]
* [[RD-8 (rocketmesin engineroket)|RD-8]]
* [[S1.5400]]
|group4 = China
Baris 86:
|group4 = Semi-cryogenic <br/>(Other)
|list4 = {{Navbox subgroup|groupstyle=width:9em;|liststyle = width:auto;
|group1 = [[Unsymmetrical dimethylhydrazine|UDMH]]/[[LiquidOksigen oxygencair|LOX]]
|list1 =
* [[RD-119]]
}}
|group5 = [[HypergolicHipergolik (propelan)|Hipergolik]]
|list5 = {{Navbox subgroup|groupstyle=width:10em;|liststyle = width:auto;
|group1 = [[Aerozine 50]]/[[Dinitrogen tetroxidetetroksida|N<sub>2</sub>O<sub>4</sub>]]
|list1 =
* [[AJ10]]
* [[:en:Astris (rocket engine)|Astris]]
* [[LR-87]]
* [[LR-91]]
|group2 = [[UH 25]]/[[Dinitrogen tetroxidetetroksida|N<sub>2</sub>O<sub>4</sub>]]
|list2 =
* [[Viking (rocketmesin engineroket)|Viking]]
|group3 = [[Unsymmetrical dimethylhydrazine|UDMH]]/[[Dinitrogen tetroxidetetroksida|N<sub>2</sub>O<sub>4</sub>]]
|list3 =
* [[RD-0202]]
Baris 138:
* [[YF-20]]
* [[YF-21]]
* [[:en:YF-22 (rocket engine)|YF-22]]
* [[:en:YF-23 (rocket engine)|YF-23]]
* [[YF-24]]
* [[YF-25]]
Baris 146:
* [[Vikas engine|Vikas]]
* [[Shavit|LK-4]]
|group4 = [[Monomethylhydrazine|MMH]]/[[Dinitrogen tetroxidetetroksida|N<sub>2</sub>O<sub>4</sub>]]
|list4 =
* [[Aestus]]