Templat:Mesin roket: Perbedaan antara revisi

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{{Navbox
|title = [[OrbitalMesin spaceflight|Orbitalroket]] dan motor roket [[launchkendaraan vehiclepeluncur]]s flown [[rocket engineorbital]]s and rocket motors
|listclass = hlist
|name = Rocket Engines
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|group3 = Semi-cryogenickriogenik <br/><br/> ([[RP-1]]/[[Oksigen cair|LOX]])
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|group1 = {{USA}}
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|group4 = Semi-cryogenickriogenik <br/>(OtherLainnya)
|list4 = {{Navbox subgroup|groupstyle=width:9em;|liststyle = width:auto;
|group1 = [[Unsymmetrical dimethylhydrazine|UDMH]]/[[Oksigen cair|LOX]]
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* [[YF-40]]
* [[Yuanzheng-1|YF-50D]]
* [[VikasMesin engineVikas|Vikas]]
* [[Shavit|LK-4]]
|group4 = [[Monomethylhydrazine|MMH]]/[[Dinitrogen tetroksida|N<sub>2</sub>O<sub>4</sub>]]
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|group2 = SolidBahan fuelbakar padat
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|group1 = USAmerika Serikat
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* [[Algol (rocket stage)|Algol]]
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* [[Space Shuttle Solid Rocket Booster]]
* [[Inertial Upper Stage]]
|group2 = JapanJepang
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* [[H-IIA|SRB-A]]
|group3 = EUUni Eropa
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* [[P80 (rocket stage)|P80]]
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* [[Geosynchronous Satellite Launch Vehicle#Vehicle description|S139]]
* [[Geosynchronous Satellite Launch Vehicle Mk III#Vehicle description|S200]]
|group5 = ChinaTiongkok
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* [[FG-02]]
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* [[Shavit|RSA-3]]
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|group3 = RelatedArtikel articlesterkait
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* [[ComparisonPerbandingan ofmesin roket orbital rocket engines]]
 
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