Изворни код странице Poređenje orbitalnih raketnih motora

Ova stranica je nepotpuna lista podataka i specifikacija orbitalnih [[Ракетни мотор|raketnih motora]].

== Aktuelni, predstojeći i raketni motori u razvoju ==

{| class="wikitable sortable"
|-
! Motor
! Poreklo
! Dizajner
! [[Spacecraft|Vozilo]]
! Status
! [[Multistage rocket|Korišćenje]]
! [[Rocket propellant|Pogon]]
! Ciklus napajanja
! [[Специфични импулс|Specifični impuls]] (s){{efn|name=VSL|Na nivou mora ako je označeno ''SL'', inače u vakuumu}}
! Potisak (N){{efn|name=VSL}}
! Pritisak u komori (bar)
! Masa (kg)
! Potisak:{{zwsp}} odnos težine{{efn|Težina se izračunava pri standardnoj gravitaciji.}}
! Oksidator:{{zwsp}} odnos goriva

|-
| [[Relativity Space|Aeon 1]]
|  {{Flag|SAD}}
| [[Relativity Space]]
| [[Terran 1]] 
| U razvoju
| 1st
| [[Liquid methane|CH<sub>4</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|310}}
| {{nts|86,740}} <small>(SL)</small><ref name=terran1>{{cite web |title= Terran 1 Technical Specifications |url=http://www.relativityspace.com/terran |access-date=2019-10-05|website=Relativity}}</ref>
|
|
|
| 
|-
| [[Relativity Space|Aeon 1 Vacuum]]
| {{Flag|SAD}}
| [[Relativity Space]]
| [[Terran 1]] 
| U razvoju
| 2nd
| [[Liquid methane|CH<sub>4</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|360}}
| {{nts|100,085}} <small>(SL)</small><ref name=terran1 />
|
|
|
| 
|-
| [[AJ-10|AJ-10-190]]
| {{Flag|SAD}}
| [[Aerojet]]
| [[Space Shuttle]], [[Orion (spacecraft)|Orion]]
| Aktivan
| Upper
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]/[[Monomethylhydrazine|MMH]]
| [[Pressure-fed engine|Pod pritiskom]]
| {{Nts|316}}<ref name=":1">{{cite web|url=https://www.rocket.com/sites/default/files/documents/In-Space%20Data%20Sheets%209.13.19.pdf|title=In-Space Product Data Sheets|website=Aerojet Rocketdyne|date=September 13, 2019}}</ref>
| {{Nts|26689}}<ref name=":1" />
| {{Nts|8.62}}<ref name=":1" />
| {{Nts|118}}<ref name=":1" />
| {{Nts|23.08}}
|
|-
| [[AR1 (rocket engine)|AR1]]
| {{Flag|SAD}}
| [[Aerojet Rocketdyne]]
| [[Firefly Beta|Beta]] (potential)<ref>{{cite press release|url=http://www.globenewswire.com/news-release/2019/10/18/1932085/0/en/Aerojet-Rocketdyne-and-Firefly-Aerospace-to-Provide-Flexible-Access-to-Space.html|title=Aerojet Rocketdyne and Firefly Aerospace to Provide Flexible Access to Space|date=October 18, 2019|website=Global Newswire}}</ref>
| U razvoju
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
|
| {{nts|2,200,000}} <small>(SL)</small><ref>{{cite web |url=http://www.rocket.com/ar1-booster-engine |title=AR1 Engine|access-date=2016-10-26 |archive-url=https://web.archive.org/web/20160304012636/http://www.rocket.com/ar1-booster-engine |archive-date=2016-03-04 |url-status=dead|website=Aerojet Rocketdyne}}</ref>
|
|
|
| {{nts|2.72}}
|-
| [[BE-3]]
| {{Flag|SAD}}
| [[Blue Origin]]
| [[New Shepard]]
| Aktivan
| 1st
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Combustion tap-off cycle|Combustion tap-off]]
|
| {{nts|490,000}}<ref name="blueorigin.com be-3">{{cite web|url=https://www.blueorigin.com/engines/be-3|title=BE-3|website=Blue Origin}}</ref>
|
|
|
|
|-
| [[BE-3U]]
| {{Flag|SAD}}
| [[Blue Origin]]
| [[New Glenn]]
| U razvoju
| 2nd
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Expander cycle|Expander, open]]
|
| {{nts|710,000}}<ref name="blueorigin.com be-3" />
|
|
|
|
|-
| [[BE-4]]
| {{Flag|SAD}}
| [[Blue Origin]]
| [[New Glenn]], [[Vulcan (rocket)|Vulcan]]
| U razvoju
| 1st
| [[Methane|CH<sub>4</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
|
| {{nts|2,400,000}}<!-- {{convert|550000|lbf|kN|disp=flip}} --><ref name="sn20140917">{{cite news |last1=Ferster |first1=Warren |title=ULA To Invest in Blue Origin Engine as RD-180 Replacement |url=http://www.spacenews.com/article/launch-report/41901ula-to-invest-in-blue-origin-engine-as-rd-180-replacement |archive-url=https://archive.today/20140918114236/http://www.spacenews.com/article/launch-report/41901ula-to-invest-in-blue-origin-engine-as-rd-180-replacement |url-status=dead |archive-date=September 18, 2014 |accessdate=2014-09-19 |work=Space News |date=2014-09-17 }}</ref><ref name="BE-4">{{cite web |url=http://www.blueorigin.com/media/press_release/united-launch-alliance-and-blue-origin-announce-partnership-to-develop-new |title=BE-4 |publisher=[[Blue Origin]] |accessdate=17 September 2014 |url-status=dead |archive-url=https://web.archive.org/web/20140917232046/http://www.blueorigin.com/media/press_release/united-launch-alliance-and-blue-origin-announce-partnership-to-develop-new |archive-date=17 September 2014 }}</ref>
| {{nts|134}}<ref name="ars20160309">{{cite news |last=Berger |first=Eric |url=https://arstechnica.com/science/2016/03/behind-the-curtain-ars-goes-inside-blue-origins-secretive-rocket-factory/ |title=Behind the curtain: Ars goes inside Blue Origin's secretive rocket factory |work=[[Ars Technica]] |date=2016-03-09 |accessdate=2016-03-09 }}</ref>
|
|
|
|-
| [[CE-20]]
| {{Flag|Indija}}
| [[Liquid Propulsion Systems Centre|LPSC]]
| [[Geosynchronous Satellite Launch Vehicle Mark III|GSLV Mk III]]
| Aktivan
| Upper
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|434}}
| {{nts|196,500}}
| {{nts|60.00}}
| {{nts|588}}
| {{nts|34.1}}
| {{nts|5.05}}
|-
| [[CE-7.5]]
| {{Flag|Indija}}
| [[Liquid Propulsion Systems Centre|LPSC]]
| [[GSLV#GSLV Mk II|GSLV Mk II]] 
| Aktivan
| Upper
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged]]
| {{nts|454}}<ref name="CE7.5">{{cite web | url=http://www.spaceflight101.com/gslv-launch-vehicle-information.html | title=GSLV Launch Vehicle Information | accessdate=6 January 2014|website=Spaceflight101.com|archive-url=https://web.archive.org/web/20140106133259/http://www.spaceflight101.com/gslv-launch-vehicle-information.html|archive-date=January 6, 2014|url-status=dead}}</ref>
| {{nts|73,500}}
| {{nts|58}}
| {{nts|445}}
| {{nts|16.85}}
|
|-
| [[E2 (rocket engine)|E2]]
| {{Flag|SAD}}
| [[ABL Space Systems]]
| [[RS1 (rocket)|RS1]]
| U razvoju
| 1st
| [[RP-1]] / [[LOX]]
| [[Gas-generator cycle|Gas generator]]
| 
| {{nts|53,800}}<ref name="RS1">{{cite web|url=https://ablspacesystems.com/rs1/|title=RS1|website=ABL|language=en-US|access-date=2022-08-21}}</ref>
|
|
|
|
|-
| [[E2 Vacuum (rocket engine)|E2 Vacuum]]
| {{Flag|SAD}}
| [[ABL Space Systems]]
| [[RS1 (rocket)|RS1]]
| U razvoju
| 2nd
| [[RP-1]] / [[LOX]]
| [[Gas-generator cycle|Gas generator]]
| 
| {{nts|57,800}}<ref name="RS1" />
|
|
|
|
|-
| [[Engine-2]]
| {{Flag|SAD}}
| [[Launcher Space]]
| [[Rocket-1]]
| U razvoju
| 1st
| [[RP-1]] / [[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|327}}<ref name=":3">{{cite web|url=https://launcherspace.com/engine-2|title=Engine-2|website=LAUNCHER|language=en-US|access-date=2019-11-09}}</ref> <br/>{{nts|290}} <small>(SL)</small>
| {{nts|100,000}}<ref name=":3" />
|
|
|
| {{nts|2.62}}
|-
| [[Engine-2|Engine-2 Vacuum]]
| {{Flag|SAD}}
| [[Launcher Space]]
| [[Rocket-1]]
| U razvoju
| 2nd
| [[RP-1]] / [[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|365}}<ref name=":3" />
| {{nts|100,000}}<ref name=":3" />
|
|
|
| {{nts|2.62}}
|-
| [[Graphite-Epoxy Motor|GEM 63]]
| {{Flag|SAD}}
| [[Northrop Grumman]]
| [[Atlas V]]
| Aktivan
| [[Solid rocket booster|Booster]]
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{nts|279.06}} <small>(Vac)</small><ref>{{cite web
 | title       = NG Prop Catalog
 | url         = https://www.northropgrumman.com/wp-content/uploads/NG-Propulsion-Products-Catalog.pdf#page=43
 | date        = 2020-12-10
 | archive-url  = https://archive.today/20201210223443/https://www.northropgrumman.com/wp-content/uploads/NG-Propulsion-Products-Catalog.pdf
 | archive-date = 2020-12-10
}}</ref>
| {{nts|1,662,745}}<ref name=aerojet-gem63>{{cite web| title=Developing Vulcan Centaur| archive-url=https://web.archive.org/web/20190825004201/https://www.ulalaunch.com/docs/default-source/evolution/190408_ulapanel_all_compressed.pdf/|archive-date=August 25, 2019|url=https://www.ulalaunch.com/docs/default-source/evolution/190408_ulapanel_all_compressed.pdf/|url-status=live|date=April 4, 2019|website=ULA}}</ref>
|
|{{nts|49,300}} with&nbsp;fuel
|
|
|-
| [[Graphite-Epoxy Motor|GEM 63XL]]
| {{Flag|SAD}}
| [[Northrop Grumman]]
| [[Vulcan (rocket)|Vulcan]]
| U razvoju
| [[Solid rocket booster|Booster]]
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{nts|280.3}} <small>(Vac)</small><ref>{{cite web
 | title       = NG Prop Catalog
 | url         = https://www.northropgrumman.com/wp-content/uploads/NG-Propulsion-Products-Catalog.pdf#page=44
 | date        = 2020-12-10
 | archive-url  = https://archive.today/20201210223443/https://www.northropgrumman.com/wp-content/uploads/NG-Propulsion-Products-Catalog.pdf
 | archive-date = 2020-12-10
}}</ref>
| {{Nts|2025720}}<ref name=aerojet-gem63 />
|
| {{nts|53,400}} with&nbsp;fuel
|
|
|-
| [[Hadley (rocket engine)|Hadley]]
| {{Flag|SAD}}
| [[Ursa Major Technologies]]
| [[GOLauncher 1]]<ref>{{cite web|website=TMRO|title=Generation Orbit - 9.28|date=2016-09-11|url=https://www.youtube.com/watch?v=0CZ5ixpz6f8#t=45m|accessdate=2017-05-20|via=YouTube}}</ref>
|U razvoju
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
|
| {{nts|22,241}} <small>(SL)</small><ref>{{cite web|url=https://www.ursamajortechnologies.com/engines|title=The Engines|website=Ursa Major Technologies|language=en-US|access-date=2017-05-20}}</ref>
|
|
|
|
|-
| [[HM-7B]]
| {{Flag|Evropska Unija}}
| [[Snecma]]
| [[Ariane 2]], [[Ariane 3|3]], [[Ariane 4|4]], [[Ariane 5|5 ECA]]
| Aktivan
| Upper
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|446}}<ref name="HM7B_Astrium">{{cite web |url=http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/hm7b-rocket-engine.html |title=HM-7 and HM-7B Rocket Engine - Thrust Chamber |publisher=[[Airbus Defence and Space]] |access-date=1 November 2015 |url-status=dead |archive-url=https://web.archive.org/web/20150318003815/http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/hm7b-rocket-engine.html |archive-date=2015-03-18}}</ref> <br/>{{nts|310}} <small>(SL)</small><ref name="HM7B_Astronautix">{{cite encyclopedia |url=http://www.astronautix.com/h/hm7-b.html |archive-url=https://web.archive.org/web/20161227204239/http://astronautix.com/h/hm7-b.html |url-status=dead |archive-date=December 27, 2016 |title=HM7-B |first=Mark |last=Wade |encyclopedia=Encyclopedia Astronautica |access-date=10 June 2017}}</ref>
| {{nts|64,800}}<ref name="HM7B_Astrium" /><br/> {{nts|43,600}} <small>(SL)</small><ref name="HM7B_Astronautix" />
| {{nts|37}}<ref name="HM7B_Astrium" />
| {{nts|165}}<ref name="HM7B_Astrium" />
| {{nts|43.25}}
| {{nts|5}}
|-
| [[HyPER-15]]
| {{Flag|Južna Koreja}}
| [[Innospace]]
| Hanbit-Nano, -Micro, -Mini
| U razvoju
| 1st
| [[Paraffin wax|Paraffin]]&thinsp;/&thinsp;[[LOX]]
| [[Electric-pump-fed engine|Električna pumpa]]
| {{nts|292}}
| {{nts|150,000}}<ref>{{cite web|title=innospacecorp on Twitter: "Very proud and excited as we get ready to test the world's largest LOx/Paraffin Hybrid rocket engine developed for a smallsat Launcher.The HyPER-15, a 150kN Hybrid rocket engine, is scheduled to test this month at our Geumsan Engine Test Facility. Keep an eye out for our updates!"|url=https://twitter.com/innospacecorp/status/1410563047266033669|access-date=2021-07-26|website=Twitter|language=en}}</ref>
|
|
|
|
|-
| [[LE-5]]B
| {{Flag|Japan}}
| [[Mitsubishi Heavy Industries|Mitsubishi]], [[Japan Aerospace Exploration Agency|JAXA]]
| [[H-IIA]], <br />[[H-IIB]]
| Aktivan
| Upper
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Expander cycle#Expander bleed cycle|Expander, open]]
| {{nts|447}}<ref name="LE-5B">{{cite encyclopedia |url=http://www.astronautix.com/engines/le5b.htm |title=LE-5B |encyclopedia=Encyclopedia Astronautica |accessdate=13 January 2016 |url-status=dead |archive-url=https://web.archive.org/web/20161027060527/http://www.astronautix.com/engines/le5b.htm |archive-date=27 October 2016 }}</ref>
| {{nts|137,000}}
| {{nts|36.0}}
| {{nts|269}}
| {{nts|51.93}}
| {{nts|5}}
|-
| [[LE-7]]A
| {{Flag|Japan}}
| [[Mitsubishi Heavy Industries|Mitsubishi]], [[Japan Aerospace Exploration Agency|JAXA]]
| [[H-IIA]], <br />[[H-IIB]]
| Aktivan
| 1st
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged]]
| {{nts|438}}<ref name="LE-7A">{{cite encyclopedia |url=http://www.astronautix.com/engines/le7a.htm |title=LE-7A |encyclopedia=Encyclopedia Astronautica |accessdate=13 January 2016 |url-status=dead |archive-url=https://web.archive.org/web/20170228075700/http://www.astronautix.com/engines/le7a.htm |archive-date=28 February 2017 }}</ref> <br/>{{nts|338}} <small>(SL)</small><ref name="LE-7A" />
| {{nts|1,098,000}}<br/>{{nts|870,000}} <small>(SL)</small>
| {{nts|120}}
| {{nts|1,800}}
| {{nts|65.9}}
| {{nts|5.9}}
|-
|[[LE-9]]
|{{Flag|Japan}}
|[[Mitsubishi Heavy Industries|Mitsubishi]], [[Japan Aerospace Exploration Agency|JAXA]]
|[[H3 (rocket)|H-3]]
|U razvoju
|1st
|[[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
|[[Expander cycle#Expander bleed cycle|Expander, open]]
|{{nts|425}}<ref>{{Cite web |title=LE-9 |url=https://www.jaxa.jp/press/2016/06/files/20160614_h3_01_j.pdf}}</ref>
|{{nts|147,1000}}
|{{nts|100
}}
|{{nts|2400}}
|{{nts|62.5}}
|{{nts|5}}.9
|-
| [[Firefly Alpha|Lightning 1]]
| {{Flag|SAD}}
| [[Firefly Aerospace]]
| [[Firefly Alpha|Alpha]]
| Aktivan
| 2nd
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Combustion tap-off cycle|Combustion tap-off]]
| {{nts|322}}<ref name=":7">{{cite web|url=https://firefly.com/launch-alpha/|title=Launch-alpha|website=Firefly Aerospace|language=en-US|access-date=2020-02-02}}</ref>
| {{nts|70,100}}<ref name=":7" />
|
|
|
|
|-
| [[Merlin (rocket engine)#Merlin 1D|Merlin 1D FT]]
| {{Flag|SAD}}
| [[SpaceX]]
| Falcon [[Falcon 9 Block 5|9 B5]], [[Falcon Heavy|Heavy]]
| Aktivan
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|311}}
| {{nts|914,000}}<ref name="Merlin 1D Full Thrust">{{cite web | url=http://www.spacex.com/news/2013/03/26/merlin-engines | title=Merlin 1D | work=SpaceX | accessdate=26 February 2016 | url-status=dead | archive-url=https://web.archive.org/web/20150906071827/http://www.spacex.com/news/2013/03/26/merlin-engines | archive-date=6 September 2015 }}</ref> <br/>{{nts|845,000}} <small>(SL)</small><ref name="Merlin 1D Full Thrust" />
|108.0<ref>{{Cite web |title=Evolution of the SpaceX Merlin engine |url=http://www.b14643.de/Spacerockets_2/United_States_1/Falcon-9/Merlin/index.htm |access-date=2022-05-08 |website=www.b14643.de}}</ref>
| {{nts|470}}
| {{nts|194.5}}<ref name="Merlin 1D Full Thrust" />
|
|-
| [[Merlin (rocket engine)#Merlin 1D Vacuum|Merlin Vacuum 1D]]
| {{Flag|SAD}}
| [[SpaceX]]
| Falcon [[Falcon 9 Block 5|9 B5]], [[Falcon Heavy|Heavy]]
| Aktivan
| 2nd
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|348}}<ref name="Merlin Vacuum 1D">{{cite web | title=SpaceX Falcon 9 Product Page | url=http://www.spacex.com/falcon9 | accessdate=2015-11-01 | url-status=dead | archive-url=https://web.archive.org/web/20140805175724/http://www.spacex.com/falcon9 | archive-date=2014-08-05 }}</ref>
| {{nts|981,000}}<ref>{{cite web|title=SpaceX|url=http://www.spacex.com/|access-date=2020-09-24|website=SpaceX|language=en}}</ref>
|
|
|
| {{nts|2.36}}
|-
| [[M10 (rocket engine)|M10]]
| {{Flag|Evropska Unija}}
| [[Avio]]
| [[Vega-E]]<ref name="avioM10">{{cite web |url=https://www.avio.com/it/m-10 |title=Motore M10 |publisher=[[Avio]] |language=Italian |trans-title=Engine M10 |access-date=2021-03-24}}</ref>
| U razvoju
| Upper<ref name="avioM10" />
| [[Liquid methane|CH<sub>4</sub>]]&thinsp;/&thinsp;[[Liquid oxygen|LOX]]<ref name="avioM10" />
| [[Expander cycle|Expander, closed]]
| {{nts|362}}<ref name="avioM10" />
| {{nts|98,000}}<ref name="avioM10" />
|
| 
| 
| {{nts|3.4}}<ref name="avioM10" />
|-
| [[LauncherOne|NewtonThree]]
| {{Flag|SAD}}
| [[Virgin Orbit]]
| [[LauncherOne]]
| Aktivan
| [[Booster (rocketry)|Booster]]
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| Gas generator<ref name="arc.aiaa.org">{{Cite book|chapter-url=https://arc.aiaa.org/doi/pdfplus/10.2514/6.2016-4984|doi = 10.2514/6.2016-4984|chapter = Turbopump Design and Development for the Virgin Galactic Newton ''Three'' Engine System|title = 52nd AIAA/SAE/ASEE Joint Propulsion Conference|year = 2016|last1 = Sargent|first1 = Scott R.|last2 = Noall|first2 = Jeff|last3 = Becker|first3 = Matthew|last4 = MacKlin|first4 = Scott|isbn = 978-1-62410-406-0}}</ref>
|
| {{nts|266,893}}<ref name="virgingalactic1">{{cite web|url=http://www.virgingalactic.com/assets/uploads/2014/11/VG_LauncherOne_ServiceGuide_v0.2_OSR.pdf|title=LauncherOne Service Guide|archive-url=https://web.archive.org/web/20171022123920/http://www.virgingalactic.com/assets/uploads/2014/11/VG_LauncherOne_ServiceGuide_v0.2_OSR.pdf|archive-date=2017-10-22|url-status=dead}}</ref>
|
|
|
|
|-
| [[LauncherOne|NewtonFour]]
| {{Flag|SAD}}
| [[Virgin Orbit]]
| [[LauncherOne]]
| Aktivan
| 2nd
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| Gas generator<ref name="arc.aiaa.org"/>
|
| {{nts|22,241}}<ref name="virgingalactic1"/>
|
|
|
|
|-
| [[NK-33|NK-33A (AJ26-62)]], <br/><small>11Д111&thinsp;/&thinsp;14Д15</small>
| {{Flag|SSSR}}
| [[JSC Kuznetsov]]
| [[Antares 100]], [[Soyuz-2-1v]]
| Aktivan
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|331}}<ref name="NK33">{{cite encyclopedia |url=http://www.astronautix.com/engines/nk33.htm |title=NK-33 |encyclopedia=Encyclopedia Astronautica |accessdate=30 January 2014 |archive-url=https://web.archive.org/web/20020625124013/http://www.astronautix.com/engines/nk33.htm |archive-date=25 June 2002 |url-status=dead }}</ref><br/>{{nts|297}} <small>(SL)</small>
| {{nts|1,680,000}} <br/>{{nts|1,510,000}} <small>(SL)</small>
| {{nts|145}}
| {{nts|1,222}}
| {{nts|136.8}}
|
|-
| [[P80 (rocket stage)|P80]]
| {{Flag|Evropska Unija}}
| [[Avio]]
| [[Vega (rocket)|Vega]]
| Aktivan
| 1st
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{nts|280}}<ref name=":4">{{cite web|url=http://www.avio.com/en/vega/vega/vega-1-stadio-p80-motor/|title=VEGA: 1° stage - P80 Motor|website=Avio.com|language=en-US|access-date=2020-01-20}}</ref>
| {{nts|3,015,000}}<ref name=":4" />
| {{nts|88}}
| {{nts|96,000}} with&nbsp;fuel
|
|
|-
| [[P120 (rocket stage)|P120]]
| {{Flag|Evropska Unija}}
| [[Avio]]
| [[Ariane 6]], <br>[[Vega-C]]
| Aktivan
| [[Solid rocket booster|Booster]], 1st
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{nts|279}}<ref name="P120Ctestfire">[https://www.ariane.group/wp-content/uploads/2018/07/P120C-successful-testfire.pdf Press release: Successful first test firing for the P120C solid rocket motor for Ariane 6 and Vega-C]</ref>
| {{nts|4,650,000}}<ref name="P120Ctestfire" />
| {{nts|105}}
| {{nts|161,000}} with&nbsp;fuel<ref name="P120Ctestfire" />
|
|
|-
| [[Ariane 5#Solid boosters|P230]]
| {{Flag|Evropska Unija}}
| [[Avio]]
| [[Ariane 5]]
| Aktivan
| [[Solid rocket booster|Booster]]
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{nts|286}}<ref name="P230">{{cite encyclopedia | url=http://www.astronautix.com/engines/p230.htm | title=P230 | encyclopedia=Encyclopedia Astronautica | accessdate=27 December 2011 | url-status=dead | archive-url=https://web.archive.org/web/20111231025932/http://www.astronautix.com/engines/p230.htm | archive-date=31 December 2011 }}</ref> <br/>{{nts|259}} <small>(SL)</small>
| {{nts|6,996,000}} <br/>{{nts|5,860,000}} <small>(SL)</small>
| {{nts|69}}
| {{nts|269,000}} with&nbsp;fuel<ref name="P230" />
|
|
|-
| [[Polar Satellite Launch Vehicle|S139]]
| {{Flag|Indija}}
| [[Satish Dhawan Space Centre|SDSC]]
| [[PSLV]] 
| Aktivan
| 1st
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{nts|269}}<ref name="PSLV-1">{{cite web | url=http://www.astronautix.com/engines/pslv1.htm | title=PSLV-1 | accessdate=4 April 2014 | url-status=dead | archive-url=https://web.archive.org/web/20140805133000/http://astronautix.com/engines/pslv1.htm | archive-date=5 August 2014 }}</ref>
| {{nts|486,0000}}
| {{nts|58}}
| {{nts|160,200}} <br/>with fuel
|
|
|-
| [[Raptor (rocket engine family)|Raptor]]<ref name="SpaceX Raptor"/>
| {{Flag|SAD}}
| [[SpaceX]]
| [[SpaceX Starship|Starship]]
| U razvoju
and Testing
| 1st, 2nd
| [[Liquid methane|CH<sub>4</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, full-flow]]
| {{nts|350}}<ref name=youtube-makinglifemulti>{{cite web |last1=Musk |first1=Elon |url=https://www.youtube.com/watch?v=tdUX3ypDVwI&t=22m34s |website=youtube.com |title=Making Life Multiplanetary |publisher=SpaceX |accessdate=29 September 2017 |date=29 September 2017}}</ref> <br/>{{nts|327}} <small>(SL)</small>
| {{nts|2,500,000}} <small>(SL, {{abbr|est.|estimate}})</small> (goal)<ref>{{cite web |title=Raptor 2 generates more than 230 tons of thrust at sea level, up from Raptor 1’s 185 tons |url=https://twitter.com/SpaceX/status/1491964913887027201 |website=Twitter |publisher=SpaceX |accessdate=11 February 2022}}</ref><ref>{{cite web |title=Probably 250 t-F by end of year |url=https://twitter.com/elonmusk/status/1492050572505137161 |website=Twitter |publisher=Elon Musk |accessdate=11 February 2022}}</ref>
| {{nts|330}}<ref name=":0">{{Cite news|url=https://twitter.com/elonmusk/status/1295495834998513664|title=Raptor engine just reached 330 bar chamber pressure without exploding!|date=2020-08-18|language=en-US}}</ref>
| {{nts|1360|prefix=~}} (goal)<ref name="tweet15Oct19">Elon Musk on Twitter: [https://twitter.com/elonmusk/status/1183866120240955392 Max thrust version of Raptor should achieve true T/W > 170. Target is 1.5 ton engine with >260 t-F. Max Isp version should achieve ~380 sec, but T/W probably <120 due to big nozzle. These are just guesses for now.]</ref>
| {{nts|170|prefix=≥}} (goal)<ref name="tweet15Oct19"/>
| {{nts|3.6}}<ref name="DRAFT_EA-201908">{{cite web |author1=Katy Groom |author2=Rebecca Bolt |author3=Resa Cancro |author4=Patrice Hall |author5=Kandi Lawson |author6=Mark Mercadante |author7=Michelle Moore |author8=Jane Provancha |author9=Matthew Thompson |author10=Don Dankert |author11=James Brooks |author12=Daniel Czelusnaik |author13=Eva Long |title=Draft Environmental Assessment for the SpaceX Starship and Super Heavy Launch Vehicle at Kennedy Space Center (KSC) |url=https://netspublic.grc.nasa.gov/main/20190801_Final_DRAFT_EA_SpaceX_Starship.pdf |website=netspublic.grc.nasa.gov |publisher=Space Exploration Technologies Corporation |accessdate=5 August 2019 |page=250 |language=en |date=1 August 2019 |archive-url=https://web.archive.org/web/20190802123140/https://netspublic.grc.nasa.gov/main/20190801_Final_DRAFT_EA_SpaceX_Starship.pdf |archive-date=2 August 2019 |url-status=live }}</ref>
|-
| [[Raptor (rocket engine family)|Raptor Vacuum]]<ref name="SpaceX Raptor">{{cite web | url=http://www.nasaspaceflight.com/2014/03/spacex-advances-drive-mars-rocket-raptor-power/ | title=Spacex Raptor | publisher=NASA SpaceFlight | date=7 March 2014 | accessdate=2 July 2015}}</ref>
| {{Flag|SAD}}
| [[SpaceX]]
| Starship
| U razvoju
| 2nd
| [[Liquid methane|CH<sub>4</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, full-flow]]
| {{nts|380}}+<ref name="nsf20180809">
{{cite news|url=https://www.youtube.com/watch?v=zu7WJD8vpAQ&t=46m6s|title=First Private Passenger on Lunar BFR Mission|date=17 September 2018|work=YouTube|accessdate=18 August 2018}}</ref>
| {{nts|3,000,000}}<ref>{{cite web |title=Starship Update |url=https://www.youtube.com/watch?v=sOpMrVnjYeY&t=3260s |website=Youtube |publisher=SpaceX |accessdate=11 April 2020}}</ref>
| {{nts|330}}<ref name=":0" />
| {{nts|1360|prefix=~}} (goal)<ref name="tweet15Oct19"/>
| {{nts|120|prefix=≥}} (goal)<ref name="tweet15Oct19"/>
| {{nts|3.6}}<ref name="DRAFT_EA-201908"/>
|-
| [[RD-0124]], <br/><small>14Д23</small>
| {{Flag|Rusija}}
| [[KBKhA]]
| [[Soyuz-2 (rocket)#Soyuz 2.1b|Soyuz-2.1b]], <br/>[[Soyuz-2-1v]], <br/>[[Angara (rocket family)|Angara]]
| Aktivan
| 2nd, 3rd
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|359}}<ref name="RD-0124">{{cite web|url=http://www.kbkha.ru/?p=8&cat=8&prod=51|title=RD-0124 Engine|publisher=KBKha|accessdate=7 January 2016}}</ref>
| {{nts|294,300}}
| {{nts|160}}
| {{nts|520}}
| {{nts|57.7}}
|
|-
| [[RD-0146]]D
| {{Flag|Rusija}}
| [[KBKhA]]
| [[Angara (rocket family)|Angara]]
| U razvoju
| Upper
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Expander cycle|Expander, closed]]
| {{nts|470}}<ref name="RD-0146">{{cite web|url=http://www.khrunichev.ru/main.php?id=304|title=ГКНПЦ имени М.В.Хруничева {{!}} Жидкостный ракетный двигатель РД - 0146|website=www.khrunichev.ru|access-date=2019-07-27}}</ref>
| {{nts|68,600}}
| {{nts|59}}
|
|
|
|-
| [[RD-107]]A, <br/><small>14Д22</small>
| {{Flag|Rusija}}
| [[NPO Energomash]]
| [[Soyuz-FG]], [[Soyuz-2 (rocket)|-2]]
| Aktivan
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|320.2}}<ref name="RD-107A and RD-108A">{{cite web | url=http://www.npoenergomash.ru/eng/dejatelnost/engines/rd107/ | title=RD-107A and RD-108A | work=NPO Energomash | accessdate=30 June 2015}}</ref> <br/>{{nts|263.3}} <small>(SL)</small>
| {{nts|1,019,892}} <br/>{{nts|839,449}} <small>(SL)</small>
| {{nts|61.2}}
| {{nts|1,090}}
| {{nts|78.53}}
|
|-
| [[RD-107|RD-108A]], <br/><small>14Д21</small>
| {{Flag|Rusija}}
| [[NPO Energomash]]
| [[Soyuz-FG]], [[Soyuz-2 (rocket)|-2]]
| Aktivan
| 2nd
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|320.6}}<ref name="RD-107A and RD-108A" /> <br/>{{nts|257.7}} <small>(SL)</small>
| {{nts|921,825}} <br/>{{nts|792,377}} <small>(SL)</small>
| {{nts|55.5}}
| {{nts|1,075}}
| {{nts|75.16}}
|
|-
| [[RD-170 (rocket engine)|RD-171M]],{{efn|name=RD-170|Najmoćniji višekomorni raketni motor na svetu}} <small>11Д520</small>
| {{Flag|Rusija}}
| [[NPO Energomash]]
| [[Soyuz-5 (rocket)|Soyuz-5]], [[Zenit-2M]], [[Zenit-3SL|-3SL]], [[Zenit-3SLB|-3SLB]], [[Zenit-3SLBF|-3SLBF]]
| Aktivan
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|337.2}}<ref name="RD-171M">{{cite web | url=http://www.npoenergomash.ru/eng/dejatelnost/engines/rd171m/ | title=RD-171M | work=NPO Energomash | accessdate=30 June 2015}}</ref> <br/>{{nts|309.5}} <small>(SL)</small>
| {{nts|7,904,160}} <br/>{{nts|7,256,921}} <small>(SL)</small>
| {{nts|250}}
| {{nts|9,300}}
| {{nts|79.57}}
|
|-
| [[RD-180]]
| {{Flag|Rusija}}
| [[NPO Energomash]]
| [[Atlas V]], [[Atlas III|III]]
| Aktivan
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|338.4}}<ref name="RD-180">{{cite web | url=http://www.npoenergomash.ru/eng/dejatelnost/engines/rd180/ | title=RD-180 | work=NPO Energomash | accessdate=30 June 2015}}</ref> <br/>{{nts|311.9}} <small>(SL)</small>
| {{nts|4,152,136}} <br/>{{nts|3,826,555}} <small>(SL)</small>
| {{nts|261.7}}
| {{nts|5,480}}
| {{nts|71.2}}
| {{nts|2.72}}
|-
| [[RD-181]]
| {{Flag|Rusija}}
| [[NPO Energomash]]
| [[Antares 200]]
| Aktivan
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|339.2}}<ref>{{cite web|url=http://spaceflight101.com/spacerockets/antares-200-series/|title = Antares 200 Series – Rockets}}</ref> <br/>{{nts|311.9}} <small>(SL)</small>
| {{nts|2,085,000}} <br/>{{nts|1,922,000}} <small>(SL)</small>
| {{nts|262.6}}
| {{nts|2,200}}
| {{nts|89}}
|
|-
| [[RD-191]]
| {{Flag|Rusija}}
| [[NPO Energomash]]
| [[Angara (rocket family)|Angara]]
| Aktivan
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|337.5}}<ref name="RD-191">{{cite web | url=http://www.npoenergomash.ru/eng/dejatelnost/engines/rd191/ | title=RD-191 | work=NPO Energomash | accessdate=30 June 2015}}</ref> <br/>{{nts|311.2}} <small>(SL)</small>
| {{nts|2,084,894}} <br/>{{nts|1,922,103}} <small>(SL)</small>
| {{nts|262.6}}
| {{nts|2,200}}
| {{nts|89.09}}
|
|-
| [[RD-193]]
| {{Flag|Rusija}}
| [[NPO Energomash]]
| [[Soyuz-2-1v]]
| U razvoju
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|337.5}}<ref name="RD-193 Engine">{{Cite news|title = Универсальный ракетный двигатель РД-193. Мнение инженера-разработчика|url = http://novosti-kosmonavtiki.ru/mag/2013/1004/13840/|publisher = Журнал «Новости космонавтики»}}</ref> <br/>{{nts|311.2}} <small>(SL)</small>
| {{nts|2,084,894}} <br/>{{nts|1,922,103}} <small>(SL)</small>
|
| {{nts|1,900}}
| {{nts|103.15}}
|
|-
| [[RD-276]], <br/><small>14Д14М</small>
| {{Flag|Rusija}}
| [[NPO Energomash]]
| [[Proton-M]] 
| Aktivan
| 1st
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|315.8}}<ref name="RD-276">{{cite web | url=http://www.engine.space/eng/dejatelnost/engines/rd-276/ | title=RD-276 "Comrade" | work=NPO Energomash | accessdate=14 October 2019}}</ref> <br/>{{nts|288}} <small>(SL)</small>
| {{nts|1,831,882}} <br/>{{nts|1,671,053}} <small>(SL)</small>
| {{nts|168.5}}
| {{nts|1,120}}
| {{nts|171.2}}
|
|-
| [[RD-801]]
| {{Flag|Ukrajina}}
| [[Yuzhnoye Design Office|Pivdenne]]/{{zwsp}}[[Yuzhmash|Pivdenmash]]
| [[Mayak (rocket family)|Mayak]] 
| U razvoju
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|336}} <ref name="yuzhnoye.com RD-801">{{cite web|url=https://www.yuzhnoye.com/en/technique/rocket-engines/steering/rd-801/|title=RD-801|website=www.yuzhnoye.com|access-date=2020-01-19}}</ref> <br/>{{nts|300.7}} <small>(SL)</small>
| {{nts|1,339,255}} <br/>{{nts|1,198,608}} <small>(SL)</small>
| {{nts|180}}
| {{nts|1,630}}
| 
| {{nts|2.65}}
|-
| [[RD-809K]]
| {{Flag|Ukrajina}}
| [[Yuzhnoye Design Office|Pivdenne]]/{{zwsp}}[[Yuzhmash|Pivdenmash]]
| [[Mayak (rocket family)|Mayak]]
| U razvoju
| Upper
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|352}} <ref name="yuzhnoye.com RD-801" />
| {{nts|98,067}}
|
| {{nts|330}}
| 
| {{nts|2.62}}
|-
| [[RD-810]]
| {{Flag|Ukrajina}}
| [[Yuzhnoye Design Office|Pivdenne]]/{{zwsp}}[[Yuzhmash|Pivdenmash]]
| [[Mayak (rocket family)|Mayak]], [[Zenit (rocket family)|Zenit]]
| U razvoju
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|335.5}} <ref>{{cite web|url=https://www.yuzhnoye.com/en/technique/rocket-engines/steering/rd-810/|title=RD-810|website=www.yuzhnoye.com|access-date=2020-01-19}}</ref> <br/>{{nts|299}} <small>(SL)</small>
| {{nts|2,104,890}} <br/>{{nts|1,876,149}} <small>(SL)</small>
| {{nts|180}}
| {{nts|2,800}}
| 
| {{nts|2.65}}
|-
| [[RD-843]]
| {{Flag|Ukrajina}}
| [[Yuzhnoye Design Office|Pivdenne]]/{{zwsp}}[[Yuzhmash|Pivdenmash]]
| [[Vega (rocket)|Vega]] 
| Aktivan
| upper
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Pressure-fed engine|Pod pritiskom]]
| {{nts|315.5}}
| {{nts|2,452}}
| {{nts|20.4}}
| {{nts|15.93}}
| 
| {{nts|2.0}}
|-
| [[RD-861K]]
| {{Flag|Ukrajina}}
| [[Yuzhnoye Design Office|Pivdenne]]/{{zwsp}}[[Yuzhmash|Pivdenmash]]
| [[Cyclone-4M]]
| U razvoju
| 2nd
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|330}} <ref>{{cite web|url=https://www.yuzhnoye.com/en/technique/rocket-engines/marching/rd-861k/|title=RD-861K|website=www.yuzhnoye.com|access-date=2020-01-19}}</ref>
| {{nts|77,629}}
|
| {{nts|207}}
| 
| {{nts|2.41}}
|-
| [[RD-120|RD-870]]
| {{Flag|Ukrajina}}
| [[Yuzhnoye Design Office|Pivdenne]]/{{zwsp}}[[Yuzhmash|Pivdenmash]]
| [[Cyclone-4M]]
| U razvoju
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|340}} <ref>{{cite web|url=https://www.yuzhnoye.com/en/technique/rocket-engines/steering/rd-870/|website=Yuzhnoye SDO|access-date=2020-01-19|title=RD-870}}</ref> <br/>{{nts|301.5}} <small>(SL)</small>
| {{nts|876,715}} <br/>{{nts|777,667}} <small>(SL)</small>
|
| {{nts|1353}}
|
| {{nts|2.684}}
|-
| [[Firefly Alpha|Reaver 1]]
| {{Flag|SAD}}
| [[Firefly Aerospace]]
| [[Firefly Alpha|Alpha]]
| Aktivan
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Combustion tap-off cycle|Combustion tap-off]]
| {{nts|295.6}}<ref name=":7" />
| {{nts|184,000}}<ref name=":7" />
|
|
|
|
|-
| [[RL10|RL-10A-4-2]]<ref name=":2">{{cite web|url=https://www.rocket.com/files/aerojet/documents/Capabilities/PDFs/RL10%20data%20sheet%20Feb%202016.pdf|title=RL10 Data Sheet-1|date=Feb 2016|access-date=March 23, 2019|archive-url=https://web.archive.org/web/20160705071843/http://www.rocket.com/files/aerojet/documents/Capabilities/PDFs/RL10%20data%20sheet%20Feb%202016.pdf|archive-date=July 5, 2016|url-status=dead}}</ref>
| {{Flag|SAD}}
| [[Aerojet Rocketdyne]]
| Atlas [[Atlas III|IIIB]], [[Atlas V|V]]
| Aktivan
| Upper
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Expander cycle|Expander, closed]]
| {{nts|451}}
| {{nts|99,195}}
| {{nts|42}}
| {{nts|168}}
| {{nts|60.27}}
| {{nts|5.5}}
|-
| [[RL10|RL-10B-2]]<ref name=":2" />
| {{Flag|SAD}}
| [[Aerojet Rocketdyne]]
| [[Delta III]], [[Delta IV|IV]], [[Space Launch System|SLS]]
| Aktivan
| Upper
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Expander cycle|Expander, closed]]
| {{nts|465.5}}
| {{nts|110,093}}
| {{nts|44}}
| {{nts|301}}
| {{nts|37.27}}
| {{nts|5.88}}
|-
| [[RL10|RL-10C-1]]<ref name=":2" />
| {{Flag|SAD}}
| [[Aerojet Rocketdyne]]
| [[Delta III]], [[Delta IV|IV]], [[Space Launch System|SLS]], [[Vulcan (rocket)|Vulcan]]
| Aktivan
| Upper
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Expander cycle|Expander, closed]]
| {{nts|450}}
| {{nts|101,820}}
| {{nts|44}}
| {{nts|191}}
| {{nts|54.5}}
| {{nts|5.5}}
|-
| [[RS-25]]
| {{Flag|SAD}}
| [[Rocketdyne]]
| [[Space Shuttle]], [[Space Launch System|SLS]]
| Aktivan
| 1st
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, fuel-rich]]
| {{nts|452.3}} <br/>{{nts|366}} <small>(SL)</small>
| {{nts|2,279,000}} <br/>{{nts|1,860,000}} <small>(SL)</small><ref name="aerojet">Aerojet Rocketdyne, [https://www.rocket.com/rs-25-engine RS-25 Engine] {{Webarchive|url=https://web.archive.org/web/20151229215644/https://www.rocket.com/rs-25-engine |date=2015-12-29 }} (accessed July 22, 2014)</ref>
| {{nts|206.4}}
| {{nts|3,526}}
| {{nts|53.79}}
|
|-
| [[RS-68A]]{{efn|Najmoćniji motor na vodonik na svetu}}
| {{Flag|SAD}}
| [[Pratt & Whitney Rocketdyne|Rocketdyne]]
| [[Delta IV]], [[Delta IV Heavy|IV Heavy]]
| Aktivan
| 1st
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|411}}<ref name="RS-68A">{{cite web | title=RS-68A|url=https://www.rocket.com/space/liquid-engines/rs-68a | publisher=www.rocket.com|accessdate=19 January 2020}}</ref> <br/>{{nts|362}} <small>(SL)</small>
| {{nts|3,558,577}} <br/>{{nts|3,135,996}} <small>(SL)</small>
| {{nts|109}}
| {{nts|6,686}}
| {{nts|54.31}}
| {{nts|5.97}}
|-
| [[Rutherford (rocket engine)|Rutherford]]
| {{Flag|Novi Zeland}} {{Flag|SAD}}
| [[Rocket Lab]]
| [[Electron (rocket)|Electron]]
| Aktivan
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Electric-pump-fed engine|Električna pumpa]]
| {{nts|311}}
| {{nts|24,900}} <br/>{{nts|25,000}} <small>(SL)</small>
|
| {{nts|35}}<ref name="RutherfordAug20">{{cite web |title=Rocket Lab Increases Electron Payload Capacity, Enabling Interplanetary Missions and Reusability |url=https://www.rocketlabusa.com/about-us/updates/rocket-lab-increases-electron-payload-capacity-enabling-interplanetary-missions-and-reusability/ |website=Rocket Lab |accessdate=26 October 2020 |language=en}}</ref>
| {{nts|72.8}} (SL)
|
|-
| [[Rutherford (rocket engine)|Rutherford Vacuum]]
| {{Flag|Novi Zeland}} {{Flag|SAD}}
| [[Rocket Lab]]
| [[Electron (rocket)|Electron]]
| Aktivan
| 2nd
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Electric-pump-fed engine|Električna pumpa]]
| {{nts|343}}
| {{nts|25,800}}<ref name="RutherfordAug20"/>
|
|
|
|
|-
| [[GSLV Mk III#Stage 1 – solid boosters|S200]]
| {{Flag|Indija}}
| [[Satish Dhawan Space Centre|SDSC]]
| [[GSLV Mk III]] 
| Aktivan
| Booster
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{nts|274.5}}<ref name="isrolvm3">{{cite web | url=http://isro.org/launchers/lvm3 | title=LVM3 | accessdate=21 December 2014 | archive-url=https://web.archive.org/web/20150910082020/http://isro.org/launchers/lvm3 | archive-date=10 September 2015 | url-status=dead }}</ref>
| {{nts|5,150,000}}<ref name="isros200">{{cite web |url=http://www.isro.org/pressrelease/contents/2010/pdf/S200_STATIC_TEST-01.pdf |title=ISRO Press Release: S200 First Static Test (S-200-ST-01) |access-date=2015-09-25 |archive-url=https://web.archive.org/web/20130311191452/http://isro.org/pressrelease/contents/2010/pdf/S200_STATIC_TEST-01.pdf |archive-date=2013-03-11 |url-status=dead }}</ref><ref name="dnai3sb">{{cite web|url=http://www.dnaindia.com/scitech/report_isro-successfully-tests-world-s-3rd-largest-solid-booster_1338945|title=Isro successfully tests world's 3rd largest solid booster|work=dna|accessdate=4 October 2014}}</ref><ref>{{cite web|url=http://www.thehindu.com/sci-tech/article61220.ece|title=India to test world's third largest solid rocket booster|date=2009-12-07|publisher=The Hindu News Paper|work=Science and Technology Section|accessdate=2009-12-07}}</ref>
|
| {{nts|207,000}}<br/>with fuel<ref name="isrolvm3" />
|
|
|-
| [[SCE-200]]
| {{Flag|Indija}}
| [[Liquid Propulsion Systems Centre|LPSC]]
| [[GSLV Mk III]], <br/>[[Unified Launch Vehicle|ULV]]
| U razvoju
| Upper, main
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|335}} <br/>{{nts|299}} <small>(SL)</small>
| {{nts|2,030,000}} <br/>{{nts|1,820,000}} <small>(SL)</small>
| {{nts|180}}
| {{nts|2700}}
|
|
|-
| [[Space Launch System|SLS]] Solid Rocket Booster{{efn|Najveći, najmoćniji motor na čvrsto gorivo ikada napravljen}}
| {{Flag|SAD}}
| [[Orbital ATK]]
| [[Space Launch System|SLS]]
| U razvoju
| [[Solid Rocket Booster|Booster]]
| [[Polybutadiene acrylonitrile|PBAN]]
| {{n/a|Čvrsto gorivo}}
| {{nts|267}}
| {{nts|16,000,000}}
|
| {{nts|730,000}} <br/>with fuel
|
|
|-
| [[Polar Satellite Launch Vehicle|SLV-1]]
| {{Flag|Indija}}
| [[Godrej & Boyce]]
| [[PSLV]] 
| Aktivan
| Booster
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{nts|253}}<ref name="SLV-1">{{cite web| url=http://www.astronautix.com/engines/slv1.htm| title=SLV-1| accessdate=4 April 2014| url-status=dead| archive-url=https://web.archive.org/web/20140805132730/http://astronautix.com/engines/slv1.htm| archive-date=5 August 2014}}</ref>
| {{nts|502,600}}
| {{nts|43}}
| {{nts|10,800}} <br/>with fuel
|
|
|-
| [[SRB-A]]3
| {{Flag|Japan}}
| [[IHI Corporation|IHI Aerospace]], <br/>[[Japan Aerospace Exploration Agency|JAXA]]
| [[H-IIA]], <br/>[[H-IIB]], <br />[[Epsilon (rocket)|Epsilon]]
| Aktivan
| [[Solid rocket booster|Booster]]
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{nts|283.6}}<ref name="SRB-A3">{{cite web|url=http://spaceflight101.com/spacerockets/epsilon/|title=SRB-A3|work=Spaceflight101|accessdate=13 January 2016}}</ref>
| {{nts|2,305,000}} <br/>{{nts|2,150,000}} <small>(SL)</small>
| {{nts|111}}
| {{nts|76,600}} <br/>with fuel
|
|
|-

| [[TEPREL]]-B
| {{Flag|Španija}}
| [[PLD Space]]
| [[Miura 1]]
| Aktivan
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Pressure-fed engine|Pod pritiskom]]
| 
| {{nts|30,200}} <small>(SL)</small>
|
|
|
|
|-

| [[TEPREL]]-C
| {{Flag|Španija}}
| [[PLD Space]]
| [[Miura 5]]
| U razvoju
| 1st, 2nd
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas-generator]]
| 
| {{nts|190,000}} <small>(SL)</small>
|
|
|
|
|-
| [[TQ-12]]<ref>[https://mp.weixin.qq.com/s/mNVv0Pe67Ls-_53Gy2seIg “天鹊”80吨液氧甲烷发动机100%推力100秒试车圆满成功]</ref>
| {{Flag|Kina}}
| [[Landspace]]
| [[ZQ-2 (rocket)|ZQ-2]]
| Aktivan
| 1st
| [[Liquid methane|CH<sub>4</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|284}}
| {{nts|667,000}} <small>(SL)</small>
| {{nts|101}}
|
|
|
|-
| [[Vikas (rocket engine)]]
| {{Flag|Indija}}
| [[Liquid Propulsion Systems Centre|LPSC]]
| [[PSLV]], [[GSLV]], [[GSLV Mk III]]
| Aktivan
| 2nd, main, booster
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|262}}
| {{nts|680,500}}–804,500 <br/>{{nts|600,500}}–756,500 <small>(SL)</small>
| {{nts|53.0}}–58.5
|
|
|
|-
| [[Vinci (rocket engine)|Vinci]]
| {{Flag|Evropska Unija}}
| [[Snecma]]
| [[Ariane 6]]
| U razvoju
| Upper
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Expander cycle|Expander, closed]]<ref name="Vinci_Astronautix">{{cite encyclopedia |url= http://www.astronautix.com/v/vinci.html |archive-url= https://web.archive.org/web/20161027124142/http://www.astronautix.com/v/vinci.html |url-status= dead |archive-date= October 27, 2016 | title=Vinci | encyclopedia=Encyclopedia Astronautica | accessdate=10 June 2017}}</ref>
| {{nts|457}}<ref name="ArianeVinci">{{cite web|url=https://www.ariane.group/wp-content/uploads/2020/06/VINCI_2020_04_DS_EN_Eng_Web.pdf|title=Vinci® engine|publisher=Ariane|access-date=10 October 2022}}</ref>
| {{nts|180,000}}
| {{nts|60}}
| {{nts|280}}
| {{nts|65.60}}
| {{nts|6.1}}
|-
| [[Vulcain (rocket engine)|Vulcain 2]]
| {{Flag|Evropska Unija}}
| [[Snecma]]
| [[Ariane 5]]
| Aktivan
| 1st
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|429}}<ref name="Vulcain2_Astrium">{{cite web | url=http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/vulcain-2-rocket-engine.html | title=Vulcain Astrium | publisher=[[Airbus Defence and Space]] | accessdate=27 December 2011 | url-status=dead | archive-url=https://web.archive.org/web/20120327075131/http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/vulcain-2-rocket-engine.html | archive-date=2012-03-27 }}</ref> <br/>{{nts|318}} <small>(SL)</small><ref name="Vulcain2_Astronautix">{{cite encyclopedia | url= http://www.astronautix.com/v/vulcain2.html | archive-url= https://web.archive.org/web/20161228055501/http://astronautix.com/v/vulcain2.html | url-status= dead | archive-date= December 28, 2016 | title=Vulcain 2 | encyclopedia=Encyclopedia Astronautica | accessdate=27 December 2011}}</ref>
| {{nts|1,359,000}}<ref name="Vulcain2_Astrium" /> <br/>{{nts|939,500}} <small>(SL)</small><ref name="Vulcain2_Astronautix" />
| {{nts|117.3}}<ref name="Vulcain2_Astrium" />
| {{nts|1,800}}<ref name="Vulcain2_Astrium" />
| {{nts|77.04}}
|
|-
| [[YF-20|YF-21B]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 2E]], [[Long March 2F|2F]], [[Long March 3|3]]
| Aktivan
| Booster, 1st
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|260.66}}&nbsp;<small>(SL)</small><ref name="casc-lm3a-2011">{{cite book |url=http://www.cgwic.com/launchservices/download/manual/Chapter%202%20General%20Description.pdf |title=LM-3A Series Launch Vehicle User's Manual. Issue 2011 |date=2011 |publisher=[[China Aerospace Science and Technology Corporation|CASC]] |chapter=2.2 LM-3A Launch Vehicle |pages=2–4 |access-date=2016-01-16}}</ref>
| {{nts|740,400}}&nbsp;<small>(SL)</small><ref name="casc-lm3a-2011" />
|
|
|
|
|-
| [[YF-20|YF-21C]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 2C]], [[Long March 2D|2D]], [[Long March 3A|3A]], [[Long March 3B|3B]], [[Long March 3C|3C]], [[Long March 4B|4B]], [[Long March 4C|4C]]
| Aktivan
| 1st
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|260.7}}&nbsp;<small>(SL)</small><ref name="casc-lm3a-2011" />
| {{nts|740,400}}&nbsp;<small>(SL)</small><ref name="casc-lm3a-2011" />
|
|
|
|
|-
| [[YF-20|YF-25]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 3B]], [[Long March 3C|3C]]
| Aktivan
| Booster
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|260.66}}&nbsp;<small>(SL)</small><ref name="casc-lm3a-2011" />
| {{nts|740,400}}&nbsp;<small>(SL)</small><ref name="casc-lm3a-2011" />
|
|
|
|
|-
| [[YF-20|YF-22B]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 2E]], [[Long March 2F|2F]]
| Aktivan
| 2nd
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|298.0}}<ref name="casc-lm3a-2011" />
| {{nts|738,400}}
|
|
|
|
|-
| [[YF-20|YF-22C]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 2C]], [[Long March 2D|2D]], [[Long March 4B|4B]], [[Long March 4C|4C]]
| Aktivan
| 2nd
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|298.0}}<ref name="casc-lm3a-2011" />
| {{nts|742,040}}
|
|
|
|
|-
| [[YF-20|YF-22D]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 3]]
| Aktivan
| 2nd
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|298.0}}<ref name="casc-lm3a-2011" />
| {{nts|741,400}}
|
|
|
|
|-
| [[YF-20|YF-22E]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 3A]], [[Long March 3B|3B]], [[Long March 3C|3C]]
| Aktivan
| 2nd
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|298.0}}<ref name="casc-lm3a-2011" />
| {{nts|741,400}}
|
|
|
|
|-
| [[YF-40]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 4B]], [[Long March 4C|4C]]
| Aktivan
| 3rd
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|303}}
| {{nts|103,000}}
|
|
|
|
|-
| [[Yuanzheng-1|YF-50D]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 3B]], [[Long March 3C|3C]], [[Long March 5|5]], [[Long March 7|7]]
| Aktivan
| Upper
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Pressure-fed engine|Pod pritiskom]]
| {{nts|315.5}}
| {{nts|6,500}}
|
|
|
|
|-
| [[YF-73]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 3]]
| Aktivan
| 3rd
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|420.0}}
| {{nts|44,150}}
|
|
|
|
|-
| [[YF-75]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 3A]], [[Long March 3B|3B]], [[Long March 3C|3C]]
| Aktivan
| 3rd
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|438.0}}<ref name="casc-lm3a-2011" />
| {{nts|78,450}}
|
|
|
|
|-
| [[YF-75D]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 5]]
| Aktivan
| 2nd
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Expander cycle|Expander, closed]]
| {{nts|442.6}}
| {{nts|88,360}}
| {{nts|41}}
| {{nts|265}}
| {{nts|34}}
| {{nts|6.0}}
|-
| [[YF-77]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 5]]
| Aktivan
| 1st
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|428}} <br/>{{nts|316.7}} <small>(SL)</small>
| {{nts|700,000}} <br/>{{nts|518,000}} <small>(SL)</small>
| {{nts|102}}
| {{nts|1,054}}
| {{nts|50}}
| {{nts|5.5}}
|-
| [[YF-79]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 9]]
| U razvoju
| 3rd
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Expander cycle|Expander, closed]]
| {{nts|455.2}}
| {{nts|250,000}}
| {{nts|70}}
|
| 
| {{nts|6.0}}
|-
| [[YF-90]]<ref>{{Cite web |url=http://hjtjnew.paperopen.com/upload/html/m/202202002.html|title=220tf补燃循环氢氧发动机研制进展|author=孙纪国,郑孟伟,龚杰峰,陶瑞峰 |date=2022-01-15 |publisher=《火箭推进》2022年02期 |language=zh-hans |accessdate=2022-06-05 }}</ref>
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 9]]
| U razvoju
| 2nd
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, fuel-rich]]
| {{nts|453}}
| {{nts|2,200,000}}
| {{nts|183}}
| {{nts|4,800}}
| {{nts|46.74}}
| {{nts|6.0}}
|-
| [[YF-100]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 7]], [[Long March 5|5]]
| Aktivan
| 1st
| RP-1/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|335.1}} <br />{{nts|300}}<small>(SL)</small>
| {{nts|1,339,480}} <br>1,199,190 <small>(SL)</small>
| {{nts|180}}
| {{nts|1,912}}
| {{nts|64}}
| {{nts|2.6}}
|-
| [[YF-115]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 6]], [[Long March 7|7]]
| Aktivan
| 2nd
| RP-1/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|341.5}} 
| {{nts|182,400}}
| {{nts|120}}
|
| 
| {{nts|2.5}}
|-
| [[YF-130]]
| {{Flag|Kina}}
| [[Academy of Aerospace Liquid Propulsion Technology|AALPT]]
| [[Long March 9]]
| U razvoju
| 1st
| RP-1/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|308}} <small>(SL)</small>
| ~{{nts|5000,000}}<small>(SL)</small>
| {{nts|220}}
| ~{{nts|6,500}}
| {{nts|78}}
| {{nts|2.62}}
|-
| [[Zefiro (rocket stage)|Zefiro 9A]]
| {{Flag|Evropska Unija}}
| [[Avio]]
| [[Vega (rocket)|Vega]]
| Aktivan
| 3rd
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{Nts|295.2}}<ref name=":5">{{cite web|url=http://www.avio.com/en/vega/vega-c/vega-c-3-stadio-zefiro-9/|title=VEGA C: 3° stage - zefiro 9|website=Avio.com|language=en-US|access-date=2020-01-20}}</ref>
| {{nts|314,000}}<ref name=":5" />
| {{nts|75}}
| {{nts|11,400}} with fuel
|
|
|-
| [[Zefiro (rocket stage)|Zefiro 23]]
| {{Flag|Evropska Unija}}
| [[Avio]]
| [[Vega (rocket)|Vega]]
| Aktivan
| 2nd
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{Nts|287.5}}<ref name=":6">{{cite web|url=http://www.avio.com/en/vega/vega/vega-2-stadio-zefiro-23/|title=VEGA: 2° stage - zefiro 23|website=Avio.com|language=en-US|access-date=2020-01-20}}</ref>
|{{Nts|1,122,000}}<ref name=":6" />
| {{nts|94}}
| {{nts|25,935}} with fuel
|
|
|-
| [[Zefiro (rocket stage)|Zefiro 40]]
| {{Flag|Evropska Unija}}
| [[Avio]]
| [[Vega-C]]
| Aktivan
| 3rd
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{Nts|293.5}}<ref name=":17">{{cite web|url=https://www.avio.com/zefiro-40/|title=Zefiro 40 Motor Main Characteristics|website=Avio.com|language=en-US|access-date=2021-05-24}}</ref>
| {{nts|1,304,000}}<ref name=":17" />
| {{nts|115}}
| {{nts|39,206}} with fuel
|
|
|} <!-- End table of active rocket engines -->

== Penzionisani i otkazani raketni motori ==

{| class="wikitable sortable"
|-
! Motor
! Poreklo
! Dizajner
! [[Spacecraft|Vozilo]]
! [[Multistage rocket|Korišćenje]]
! [[Rocket propellant|Pogon]]
! Ciklus napajanja
! [[Specifični impuls]] (s){{efn|name=VSL|Na nivou mora ako je označeno ''SL'', inače u vakuumu}}
! [[Potisak]] (N){{efn|name=VSL}}
! Masa (kg)
! Potisak:{{zwsp}} odnos težine{{efn|Težina se izračunava pri standardnoj gravitaciji.}}
! Pritisak u komori (bar)
! Oksidator:{{zwsp}} odnos goriva
|-
| [[Aerojet M-1]]
| {{Flag|SAD}}
| [[Aerojet]]
| Nova ?
| 1st, 2nd?
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|428}} <small>(SL)</small>
| {{nts|6,670,000}}
| {{nts|9,068}}
| {{nts|60}}
| {{nts|?}}
| 
|-
| [[Aestus]]
| {{nobr|{{Flag|Evropska Unija}}}}
| [[Airbus Defence and Space]]
| [[Ariane 5]] G, G+, ES
| Upper
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[Monomethylhydrazine|MMH]]
| [[Pressure-fed engine|Pod pritiskom]]
| {{nts|324}}<ref name="Aestus_Airbus">{{cite web |url= http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/aestus-rocket-engine.html |title=Aestus Rocket Engine |publisher=[[Airbus Defence and Space]] |accessdate=29 January 2014 |url-status=dead |archive-url=https://web.archive.org/web/20150420140731/http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/aestus-rocket-engine.html |archive-date=2015-04-20}}</ref>
| {{nts|30,000}}
| {{nts|111}}
| {{nts|27.6}}
| {{nts|11}}
| {{nts|1.9}}
|-
| [[Aestus II]]
| {{Flag|Evropska Unija}}
| [[Airbus Defence and Space]]
| [[Ariane 5]]
| Upper
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[Monomethylhydrazine|MMH]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|340}}<ref name="AestusII_Airbus">{{cite web |url=http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/aestus-rs72-rocket-engine.html |title=Aestus Rocket Engine |publisher=[[Airbus Defence and Space]] |accessdate=29 January 2014 |url-status=dead |archive-url=https://web.archive.org/web/20150528225225/http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/aestus-rs72-rocket-engine.html |archive-date=2015-05-28 }}</ref>
| {{nts|55,400}}
| {{nts|138}}
| {{nts|41.0}}
| {{nts|60}}
| {{nts|1.9}}
|-
| [[Aether (rocket engine)|Aether]]
| {{Flag|SAD}}
| [[Astra Space]]
| Rocket 3.0<ref>{{cite web|last=By|date=2020-02-28|title=Astra Readies Secretive Silicon Valley Rocket; Firm Exits Stealth Mode, Plans Test Launch|url=https://hackaday.com/2020/02/28/astra-readies-secretive-silicon-valley-rocket-firm-drops-out-stealth-mode-plans-test-launch-today/|access-date=2020-07-03|website=Hackaday|language=en-US}}</ref>
| 2nd
| [[RP-1]]/[[Liquid oxygen|LOX]]<ref name=":8" />
| [[Electric-pump-fed engine|Električna pumpa]]
|
|
|
|
|
|
|-
| [[AJ-60A]]
| {{Flag|SAD}}
| [[Aerojet]]
| [[Atlas V]]
| [[Solid rocket booster|Booster]]
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{nts|275}}
| {{nts|1,270,000}}<ref name=aerojet-aj60a>{{cite web|title=Atlas V Solid Rocket Motor|url=http://www.rocket.com/atlas-v-solid-rocket-motor|website=Aerojet Rocketdyne|accessdate=2015-06-02|archive-url=https://web.archive.org/web/20170314072244/http://www.rocket.com/atlas-v-solid-rocket-motor|archive-date=2017-03-14|url-status=dead}}</ref>
|
|
|
|
|-
| [[AJ-260]]-2
| {{Flag|SAD}}
| [[Aerojet]]
| S-I stage replacement (proposed)
| 1st
| [[Polybutadiene acrylonitrile|PBAN]]
| {{n/a|Čvrsto gorivo}}
| 263 s
| 26,183,755
| 831,345, with fuel
|
|
|
|-
| [[Delphin (rocket engine)|Delphin]]
| {{Flag|SAD}}
| [[Astra Space]]
| Rocket 3.0<ref>{{cite web|date=2020-03-02|title=Astra scrubs DARPA launch challenge attempt|url=https://www.nasaspaceflight.com/2020/03/astra-darpa-launch-challenge/|access-date=2020-07-03|website=NASASpaceFlight.com|language=en-US}}</ref>
| 1st
| [[RP-1]]/[[Liquid oxygen|LOX]]<ref name=":8">{{cite web|title=Astra Space Rocket|url=https://www.spacelaunchreport.com/astra.html|access-date=2020-07-03|website=www.spacelaunchreport.com}}</ref>
| [[Electric-pump-fed engine|Električna pumpa]]
|
| {{Nts|27000}}<ref>{{cite web|last=Berger|first=Eric|date=2020-02-06|title=At Astra, failure is an option|url=https://arstechnica.com/science/2020/02/at-astra-space-failure-is-an-option/|access-date=2020-07-03|website=Ars Technica|language=en-us}}</ref>
|
|
|
|
|-
| [[F-1 (rocket engine)|F-1]]{{efn|Najmoćniji raketni motor sa jednom komorom na tečno gorivo ikada razvijen}}
| {{Flag|SAD}}
| [[Rocketdyne]]
| [[Saturn V]]
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|304}} <br/>{{nts|263}} <small>(SL)</small>
| {{nts|7,770,000}} <br/>{{nts|6,770,000}} <small>(SL)</small>
| {{nts|8,391}}
| {{nts|82.27}}
| {{nts|70}}
| {{nts|2.27}}
|- 
| [[F-1 (rocket engine)|F-1A]]{{efn|Testirano, ali nikada nije leteo}}<ref>[https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19930019136.pdf Alternate Propulsion Subsystem Concepts NAS8-39210 DCN 1-1-PP-02147]</ref>
| {{Flag|SAD}}
| [[Rocketdyne]]
|
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|303}} <br/>{{nts|270}} <small>(SL)</small>
| {{nts|8,989,000}} <br/>{{nts|8,007,000}} <small>(SL)</small>
| {{nts|9,015}}
| {{nts|90.6}}
| {{nts|80}}
| {{nts|2.27}}
|- 
| [[Bristol Siddeley Gamma|Gamma 2]]
| {{Flag|Velika Britanija}}
| [[Bristol Siddeley]]
| [[Black Arrow]]
| 2nd
| [[RP-1]]&thinsp;/&thinsp;[[hydrogen peroxide|H<sub>2</sub>O<sub>2</sub>]]
| Staged, decomposition and combustion
| {{nts|265}}<ref name="Gamma2">{{cite encyclopedia |url=http://www.astronautix.com/engines/gamma2.htm |title=Gamma 2 |archive-url=https://web.archive.org/web/20130522155041/http://www.astronautix.com/engines/gamma2.htm |archive-date=22 May 2013 |encyclopedia=Encyclopedia Astronautica |accessdate=26 April 2013 |url-status=dead }}</ref>
| {{nts|68,200}}
| {{nts|173}}
| {{nts|40.22}}
|
| {{nts|8}}
|- 
| [[Bristol Siddeley Gamma|Gamma 8]]
| {{Flag|Velika Britanija}}
| [[Bristol Siddeley]]
| [[Black Arrow]]
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[hydrogen peroxide|H<sub>2</sub>O<sub>2</sub>]]
| Staged, decomposition and combustion
| {{nts|265}}<ref name="Gamma8">{{cite encyclopedia |url=http://www.astronautix.com/engines/gamma8.htm |title=Gamma 8 |archive-url=https://web.archive.org/web/20130522155114/http://www.astronautix.com/engines/gamma8.htm |archive-date=22 May 2013 |encyclopedia=Encyclopedia Astronautica |accessdate=26 April 2013 |url-status=dead }}</ref>
| {{nts|234,800}}
| {{nts|342}}
| {{nts|70.01}}
| {{nts|47.40}}
| {{nts|8}}
|-
| [[HM-7B|HM-7A]]
| {{Flag|Evropska Unija}}
| [[Snecma]]
| [[Ariane 1]]
| 3rd
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|443}}<ref name="HM7A">{{cite encyclopedia |url=http://www.astronautix.com/h/hm7-a.html |archive-url=https://web.archive.org/web/20161221093730/http://www.astronautix.com/h/hm7-a.html |url-status=dead |archive-date=December 21, 2016 |title=HM7-A |first=Mark |last=Wade |encyclopedia=Encyclopedia Astronautica |access-date=10 June 2017}}</ref> <br/>{{nts|308}} <small>(SL)</small>
| {{nts|61,700}}
| {{nts|149}}
| {{nts|42.2}}
| {{nts|30}}
| {{nts|5}}
|-
| [[J-2 (rocket engine)|J-2]]
| {{Flag|SAD}}
| [[Rocketdyne]]
| [[Saturn V]], [[Saturn IB|IB]]
| 2nd, 3rd
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|421}}<ref name="J-2">{{cite encyclopedia |url=http://www.astronautix.com/j/j-2.html |archive-url=https://web.archive.org/web/20160719175425/http://www.astronautix.com/j/j-2.html |url-status=dead |archive-date=July 19, 2016 |title=J-2 |first=Mark |last=Wade |encyclopedia=Encyclopedia Astronautica |accessdate=23 December 2011}}</ref> <br/>{{nts|200}} <small>(SL)</small>
| {{nts|1,033,100}} <br/>{{nts|486,200}} <small>(SL)</small>
| {{nts|1,438}}
| {{nts|73.18}}
| {{nts|30}}
| {{nts|5.5}}
|-
| [[J-2X]]
| {{Flag|SAD}}
| [[Pratt & Whitney Rocketdyne]]
| [[Space Launch System|SLS]] (proposed)
| Upper
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|448}}<ref name="J-2X">{{cite web |url= http://www.pw.utc.com/products/pwr/propulsion_solutions/j-2x.asp |title=J-2X Engine |publisher=Pratt & Whitney Rocketdyne |accessdate=23 December 2011 |url-status=dead |archive-url=https://web.archive.org/web/20120103030859/http://www.pw.utc.com/products/pwr/propulsion_solutions/j-2x.asp |archive-date=2012-01-03}}</ref>
| {{nts|{{convert|294,000|lbf|disp=number}}}}
| {{nts|{{convert|5,450|lb|disp=number}}}}
| {{nts|58.41}}
| {{nts|{{convert|1380|psi|bar|disp=number}}}}
| {{nts|5.5}}–4.5
|-
| [[Kestrel (rocket engine)|Kestrel]]
| {{Flag|SAD}}
| [[SpaceX]]
| [[Falcon 1]]
| Upper
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Pressure fed]]
| {{nts|317}}
| {{nts|31,000}}
| {{nts|52}}
| {{nts|65}}
| {{nts|9.3}}
| 
|-
| [[LE-5]]
| {{Flag|Japan}}
| [[Mitsubishi Heavy Industries|Mitsubishi]], [[National Space Development Agency of Japan|NASDA]]
| [[H-I]]
| Upper
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|450}}<ref name="LE-5">{{cite encyclopedia |url=http://www.astronautix.com/engines/le5.htm |title=LE-5 |encyclopedia=Encyclopedia Astronautica |accessdate=13 January 2016 |url-status=dead |archive-url=https://web.archive.org/web/20161027123109/http://www.astronautix.com/engines/le5.htm |archive-date=27 October 2016 }}</ref>
| {{nts|103,000}}
| {{nts|245}}
| {{nts|42.87}}
| {{nts|36.0}}
| {{nts|5.5}}
|-
| [[LE-5]]A
| {{Flag|Japan}}
| [[Mitsubishi Heavy Industries|Mitsubishi]], [[National Space Development Agency of Japan|NASDA]]
| [[H-II]]
| Upper
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Expander cycle#Expander bleed cycle|Expander, open]]
| {{nts|452}}<ref name="LE-5A">{{cite encyclopedia |url=http://www.astronautix.com/engines/le5a.htm |title=LE-5A |encyclopedia=Encyclopedia Astronautica |accessdate=13 January 2016 |url-status=dead |archive-url=https://web.archive.org/web/20160311185707/http://www.astronautix.com/engines/le5a.htm |archive-date=11 March 2016 }}</ref>
| {{nts|121,500}}
| {{nts|242}}
| {{nts|51.19}}
| {{nts|40.0}}
| {{nts|5}}
|-
| [[LE-7]]
| {{Flag|Japan}}
| [[Mitsubishi Heavy Industries|Mitsubishi]], [[National Space Development Agency of Japan|NASDA]]
| [[H-II]]
| 1st
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion]]
| {{nts|446}}<ref name="LE-7">{{cite encyclopedia |url=http://www.astronautix.com/engines/le7.htm |title=LE-7 |encyclopedia=Encyclopedia Astronautica |accessdate=13 January 2016 |url-status=dead |archive-url=https://web.archive.org/web/20160311183629/http://www.astronautix.com/engines/le7.htm |archive-date=11 March 2016 }}</ref>
| {{nts|1,078,000}} <br/>{{nts|843,500}} <small>(SL)</small>
| {{nts|1,714}}
| {{nts|64.13}}
| {{nts|127}}
| {{nts|5.9}}
|-
| [[Merlin (rocket engine)#Merlin 1D|Merlin 1D]]
| {{Flag|SAD}}
| [[SpaceX]]
| [[Falcon 9 v1.1]]
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|311}}<ref name="spacexfalcon9Merlinpage">{{cite web | url=http://www.spacex.com/falcon9.php#merlin_engine | title=Merlin section of Falcon 9 page | publisher=SpaceX | accessdate=2012-10-16 | archive-url=https://web.archive.org/web/20130715094112/http://www.spacex.com/falcon9 | archive-date=2013-07-15}}</ref> <br/>{{nts|282}} <small>(SL)</small><ref name="spacexfalcon9Merlinpage" />
| {{nts|723,000}}
| {{nts|470}}
| {{nts|158}}
| {{nts|97}}
| {{nts|2.34}}
|-
| [[Merlin (rocket engine)#Merlin Vacuum (1C)|Merlin Vacuum 1C]]
| {{Flag|SAD}}
| [[SpaceX]]
| [[Falcon 1]], [[Falcon 9|9]]
| 2nd
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|336}}<ref name="merlin 1c falcon9">{{cite web | url=http://www.spacelaunchreport.com/falcon9.html | title=Falcon 9 Space Launch Report | publisher=SpaceLaunchReport | accessdate=2015-11-01}}</ref>
| {{nts|413,644}}<ref name="merlin 1c falcon9" />
|
| {{nts|92}}
|
|
|-
| [[RD-0120]] <br/><small>11Д122</small>
| {{Flag|SSSR}}
| [[KBKhA]]
| [[Energia (rocket)|Energia]]
| 1st
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| Staged, fuel-rich
| {{nts|455}}<ref name="RD-0120">{{cite web |url=http://www.kbkha.ru/?p=8&cat=8&prod=34 |title= RD0120 |publisher=KBKhA}}</ref>
| {{nts|1,962,000}} <br/>{{nts|1,526,000}} <small>(SL)</small>
| {{nts|3,450}}
| {{nts|57.80}}
| {{nts|219}}
|
|-
| [[RD-8]], <br/><small>11D513</small>
| {{Flag|SSSR}}
| [[Yuzhnoye Design Office|Pivdenne]]/{{zwsp}}[[Yuzhmash|Pivdenmash]]
| [[Zenit (rocket family)|Zenit]] 
| 2nd vernier
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Staged combustion cycle|Staged, oxidizer-rich]]
| {{nts|342}}
| {{nts|78,450}}
| {{nts|356}}
|
| {{nts|77.47}}
| {{nts|2.4}}
|-
| [[KVD-1|RD-56 (KVD-1)]] <br/><small>11Д56У</small>
| {{Flag|Rusija}}
| [[KBKhM]]
| [[GSLV#GSLV Mk I (a)|GSLV Mk I]]
| Upper
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| Staged, fuel-rich
| {{nts|462}}<ref name="KVD1">{{cite web | script-title=ru:Двигатель КВД1 | url=http://kbhmisaeva.ru/main.php?id=54 | title=KVD1 Rocket Engine | publisher=КБХМ им. A.M. Исаева | language=ru}}</ref>
| {{nts|69,626}}
| {{nts|282}}
| {{nts|25.17}}
| {{nts|55.9}}
|
|-
| [[RD-107|RD-117]] <br/><small>11Д511</small>
| {{Flag|SSSR}}
| [[NPO Energomash]]
| [[Soyuz-U]]
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| Gas generator
| {{nts|316}}<ref name="lpre">{{cite web |url=http://www.lpre.de/energomash/RD-107/index.htm |title=RD-117 |work=Liquid Propellant Rocket Engines |accessdate=27 November 2012 |url-status=dead |archive-url=https://web.archive.org/web/20120826123612/http://www.lpre.de/energomash/RD-107/index.htm |archive-date=26 August 2012 }}</ref> <br/>{{nts|253}} <small>(SL)</small>
| {{nts|978,000}} <br/>{{nts|778,648}} <small>(SL)</small>
| {{nts|1,100}}
| {{nts|72.18}}
| {{nts|54.2}}
|
|-
| [[RD-107|RD-118]] <br/><small>11Д512</small>
| {{Flag|SSSR}}
| [[NPO Energomash]]
| [[Soyuz-U]]
| 2nd
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| Gas generator
| {{nts|314}}<ref name="lpre" /> <br/>{{nts|257}} <small>(SL)</small>
| {{nts|1,000,278}} <br/>{{nts|818,855}} <small>(SL)</small>
| {{nts|1,100}}
| {{nts|75.91}}
| {{nts|59.7}}
|
|-
| [[RD-170 (rocket engine)|RD-170]]{{efn|Najmoćniji raketni motor na svetu na tečno gorivo}}<small>11Д521</small><ref name="RD-170">{{cite encyclopedia |url= http://www.astronautix.com/r/rd-170.html |archive-url= https://web.archive.org/web/20160808152705/http://www.astronautix.com/r/rd-170.html |url-status= dead |archive-date= August 8, 2016 |title=RD-170 |encyclopedia=Encyclopedia Astronautica |accessdate=24 September 2019}}</ref>
| {{Flag|SSSR}}
| [[NPO Energomash]]
| [[Energia (rocket)|Energia]]
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| Staged, oxidizer-rich
| {{nts|337.2}} <br/>{{nts|309.5}} <small>(SL)</small>
| {{nts|7,904,160}} <br/>{{nts|7,256,921}} <small>(SL)</small>
| {{nts|9,300}}
| {{nts|79.57}}
| {{nts|250}}
|
|-
| [[RD-264]] <br/><small>11Д119</small>
| {{Flag|SSSR}}
| [[NPO Energomash]]
| [[Dnepr (rocket)|Dnepr]] 
| 1st
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| Staged, oxidizer-rich
| {{nts|318}}<ref name="RD-264">{{cite encyclopedia |url=http://www.astronautix.com/r/rd-264.html |archive-url=https://web.archive.org/web/20161014095858/http://www.astronautix.com/r/rd-264.html |url-status=dead |archive-date=October 14, 2016 |title=RD-264 |first=Mark |last=Wade |encyclopedia=Encyclopedia Astronautica |accessdate=10 June 2017}}</ref> <br/>{{nts|293}} <small>(SL)</small>
| {{nts|4,521,000}}
| {{nts|3,600}}
| {{nts|128.15}}
| {{nts|206}}
|-
| [[RD-275]] <br/><small>14Д14</small>
| {{Flag|Rusija}}
| [[NPO Energomash]]
| [[Proton-M]] 
| 1st
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| Staged, oxidizer-rich
| {{nts|316}}<ref name="RD-275">{{cite web | url=http://www.npoenergomash.ru/eng/dejatelnost/engines/rd253/ | title=RD-253 and RD-275 | work=NPO Energomash | accessdate=30 June 2015 | archive-url=https://web.archive.org/web/20150405185423/http://www.npoenergomash.ru/eng/dejatelnost/engines/rd253/ | archive-date=April 5, 2015 | url-status=dead }}</ref> <br/>{{nts|287}} <small>(SL)</small>
| {{nts|1,831,882}} <br/>{{nts|1,671,053}} <small>(SL)</small>
| {{nts|1,070}}
| {{nts|171.2}}
| {{nts|160.0}}
|
|-
| [[RD-854]] <br/><small>8D612</small>
| {{Flag|SSSR}}
| [[Yuzhnoye Design Office|Pivdenne]]/{{zwsp}}[[Yuzhmash|Pivdenmash]]
| [[R-36ORB]]
| 3rd
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| Gas generator
|
|
|
|
|
|-
| [[RD-855]] <br/><small>8D68M</small>
| {{Flag|SSSR}}
| [[Yuzhnoye Design Office|Pivdenne]]/{{zwsp}}[[Yuzhmash|Pivdenmash]]
| [[Tsyklon-2]], [[Tsyklon-3|-3]], [[R-36 (missile)|R-36]]
| 1st vernier
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| Gas generator
| 
| {{nts|328,000}}
| {{nts|320}}
| 
| {{nts|65.70}}
| {{nts|1.97}}
|-
| [[RD-856]] <br/><small>8D69M</small>
| {{Flag|SSSR}}
| [[Yuzhnoye Design Office|Pivdenne]]/{{zwsp}}[[Yuzhmash|Pivdenmash]]
| [[Tsyklon-2]], [[Tsyklon-3|-3]] ([[Tsyklon-4|-4]]), [[R-36 (missile)|R-36]]
| 2nd vernier
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| Gas generator
| 
| {{nts|54,230}}
| {{nts|112.5}}
| 
| {{nts|71.60}}
| {{nts|1.98}}
|-
| [[RD-861]] <br/><small>11D25</small>
| {{Flag|SSSR}}
| [[Yuzhnoye Design Office|Pivdenne]]/{{zwsp}}[[Yuzhmash|Pivdenmash]]
| [[Tsyklon-2]], [[Tsyklon-3|-3]]
| 3rd
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| Gas generator
| 
| {{nts|78,710}}
| {{nts|123}}
| 
| {{nts|88.8}}
| {{nts|2.1}}
|-
| [[RD-864]] <br/><small>15D177</small>
| {{Flag|SSSR}}
| [[Yuzhnoye Design Office|Pivdenne]]/{{zwsp}}[[Yuzhmash|Pivdenmash]]
| [[R-36M|R-36 (missile)]], [[Dnepr (rocket)|Dnipro]] 
| 3rd
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| Gas generator
| {{ntsh|309}}298–309
| {{ntsh|20,200}}8,450–20,200
| {{nts|199}}
| 
| {{ntsh|41}}17–41
| {{nts|1.8}}
|-
| [[RD-869]] <br/><small>15D300</small>
| {{Flag|SSSR}}
| [[Yuzhnoye Design Office|Pivdenne]]/{{zwsp}}[[Yuzhmash|Pivdenmash]]
| [[R-36M]]
| 3rd
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| Gas generator
| {{ntsh|313}}302.3–313
| {{ntsh|20,470}}8,580–20,470
| {{nts|196}}
| 
| {{ntsh|41}}17–41
| {{nts|1.8}}
|-
| [[RS-27A]]
| {{Flag|SAD}}
| [[Rocketdyne]]
| [[Delta (rocket family)|Delta]]
| 1st
| [[RP-1]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|302}}<ref name="RS-27A">{{cite encyclopedia |url=http://www.astronautix.com/r/rs-27a.html |archive-url=https://web.archive.org/web/20160825210024/http://www.astronautix.com/r/rs-27a.html |url-status=dead |archive-date=August 25, 2016 |title=RS-27A |encyclopedia=Encyclopedia Astronautica |accessdate=2 November 2021}}</ref> <br/>{{nts|255}} <small>(SL)</small>
| {{nts|1,054,200}}
| {{nts|1091}}
| {{nts|102.5}}
| {{nts|49}}
| {{nts|2.245}}
|-
| [[Space Shuttle Solid Rocket Booster]]{{efn|Najveći raketni motor na čvrsto gorivo koji je ikada leteo, i prvi koji se koristio za primarni pogon u svemirskim misijama sa ljudskom posadom }}
| {{Flag|SAD}}
| [[Thiokol]]
| [[Space Shuttle]], [[Ares I]]
| [[Solid Rocket Booster|Booster]]
| [[Polybutadiene acrylonitrile|PBAN]]&thinsp;/&thinsp;[[APCP]]
| {{n/a|Čvrsto gorivo}}
| {{nts|268}}
| {{nts|14,000,000}} <br/>{{nts|12,500,000}} <small>(SL)</small>
| {{nts|590,000}} <br/>with fuel
|
|
|
|-
| [[SRB-A]]
| {{Flag|Japan}}
| [[IHI Corporation|IHI Aerospace]], [[Japan Aerospace Exploration Agency|JAXA]]
| [[H-IIA]]
| [[Solid rocket booster|Booster]]
| [[HTPB]]
| {{n/a|Čvrsto gorivo}}
| {{nts|280}}<ref name="SRB-A">{{cite encyclopedia |url=http://www.astronautix.com/engines/srba.htm |archive-url=https://web.archive.org/web/20020301084629/http://www.astronautix.com/engines/srba.htm |url-status=dead |archive-date=March 1, 2002 |title=SRB-A |encyclopedia=Encyclopedia Astronautica |accessdate=13 January 2016}}</ref>
| {{nts|2,250,000}}
| {{nts|76,400}} with fuel
|
|
|
|-
| [[UA120]]7
| {{Flag|SAD}}
| [[United Technologies]]
| [[Titan IV]]
| [[Solid Rocket Booster|Booster]]
| [[Polybutadiene acrylonitrile|PBAN]]
| {{n/a|Čvrsto gorivo}}
| {{nts|272}}<ref name="UA1207">{{cite encyclopedia |url=http://www.astronautix.com/engines/ua1207.htm |title=UA1207 |archive-url=https://web.archive.org/web/20160304000325/http://www.astronautix.com/engines/ua1207.htm |archive-date=4 March 2016 |encyclopedia=Encyclopedia Astronautica |accessdate=27 December 2015 |url-status=dead }}</ref> <br/>{{nts|245}} <small>(SL)</small>
| {{nts|7,116,000}} <br/>{{nts|6,410,400}} <small>(SL)</small>
| {{nts|319,330}} <br/>with fuel
|
|
|
|-
| [[Viking (rocket engine)|Viking 2]]
| {{Flag|Evropska Unija}}
| [[Snecma]]
| [[Ariane 1]]
| 1st
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Gas-generator cycle|Gas generator]]
|
| {{nts|690,000}} <br/>{{nts|611,200}} <small>(SL)</small>
| {{nts|776}}
| {{nts|90.67}}
|
|
|-
| [[Viking (rocket engine)|Viking 2B]]
| {{Flag|Evropska Unija}}
| [[Snecma]]
| [[Ariane 2]], [[Ariane 3|3]]
| 1st
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UH 25|UH&thinsp;25]]
| [[Gas-generator cycle|Gas generator]]
|
| {{nts|643,000}} <small>(SL)</small>
| {{nts|776}}
| {{nts|84.5}}
|
|
|-
| [[Viking (rocket engine)|Viking 4]]
| {{Flag|Evropska Unija}}
| [[Snecma]]
| [[Ariane 1]]
| 2nd
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UDMH]]
| [[Gas-generator cycle|Gas generator]]
|
| {{nts|713,000}}
| {{nts|826}}
| {{nts|88}}
|
|
|-
| [[Viking (rocket engine)|Viking 4B]]
| {{Flag|Evropska Unija}}
| [[Snecma]]
| [[Ariane 2]], [[Ariane 3|3]], [[Ariane 4|4]]
| 2nd
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UH 25|UH&thinsp;25]]
| [[Gas-generator cycle|Gas generator]]
|
| {{nts|800,000}}
| {{nts|826}}
| {{nts|98.76}}
|
|
|-
| [[Viking (rocket engine)|Viking 5C]]
| {{Flag|Evropska Unija}}
| [[Snecma]]
| [[Ariane 4]]
| 1st
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UH 25|UH&thinsp;25]]
| [[Gas-generator cycle|Gas generator]]
|
| {{nts|758,000}} <br/>{{nts|678,000}} <small>(SL)</small>
| {{nts|826}}
| {{nts|93.57}}
|
|
|-
| [[Viking (rocket engine)|Viking 6]]
| {{Flag|Evropska Unija}}
| [[Snecma]]
| [[Ariane 4]]
| [[Booster (rocketry)|Booster]]
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]&thinsp;/&thinsp;[[UH 25|UH&thinsp;25]]
| [[Gas-generator cycle|Gas generator]]
|
| {{nts|750,000}}
| {{nts|826}}
| {{nts|92.59}}
|
|
|-
| [[Vulcain (rocket engine)|Vulcain]] <br/><small>HM-60</small>
| {{Flag|Evropska Unija}}
| [[Snecma]]
| [[Ariane 5]]
| 1st
| [[Liquid hydrogen|LH<sub>2</sub>]]&thinsp;/&thinsp;[[LOX]]
| [[Gas-generator cycle|Gas generator]]
| {{nts|439}}<ref name="Vulcain_Astrium">{{cite web | url=http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/vulcain-rocket-engine.html | title=Vulcain Astrium | publisher=[[Airbus Defence and Space]] | accessdate=27 December 2011 | url-status=dead | archive-url=https://web.archive.org/web/20120225051943/http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/vulcain-rocket-engine.html | archive-date=2012-02-25 }}</ref> <br/>{{nts|326}} <small>(SL)</small><ref name="Vulcain_Astronautix">{{cite encyclopedia | url= http://www.astronautix.com/v/vulcain.html | archive-url= https://web.archive.org/web/20161228033910/http://astronautix.com/v/vulcain.html | url-status= dead | archive-date= December 28, 2016 | title=Vulcain | encyclopedia=Encyclopedia Astronautica | accessdate=27 December 2011}}</ref>
| {{nts|1,113,000}}<ref name="Vulcain_Astrium" /> <br/>{{nts|773,200}} <small>(SL)</small><ref name="Vulcain_Astronautix" />
| {{nts|1,300}}<ref name="Vulcain_Astronautix" />
| {{nts|84.38}}
| {{nts|109}}<ref name="Vulcain_Astrium" />
|
|-
| [[Waxwing (Rocket motor)|Waxwing]]
| {{Flag|Velika Britanija}}
| [[Bristol Aerojet]]
| [[Black Arrow]]
| Upper
|
| {{n/a|Čvrsto gorivo}}
| {{nts|278}}<ref name="Waxwing">{{cite encyclopedia |url= http://www.astronautix.com/b/blackarrow-3.html |archive-url= https://web.archive.org/web/20161228022014/http://astronautix.com/b/blackarrow-3.html |url-status= dead |archive-date= December 28, 2016 |title=Black Arrow-3 |encyclopedia=Encyclopedia Astronautica |accessdate=26 April 2013}}</ref> <br/>{{nts|245}} <small>(SL)</small>
| {{nts|29,400}} <br/>{{nts|25,900}} <small>(SL)</small>
| {{nts|87}}
| {{nts|34.48}}
|
|
|}

== Vidi još ==

* [[Poređenje orbitalnih sistema za lansiranje]]
* [[Poređenje familija orbitalnih lansera]]
* [[Poređenje svemirskih vozila sa posadom]]
* [[Poređenje teretnih vozila svemirske stanice]]
* [[Poređenje orbitalnih sistema za lansiranje na čvrsto gorivo]]
* [[Spisak dizajna sistema za lansiranje u svemir]]
* [[Spisak orbitalnih sistema za lansiranje]]

== Napomene ==
{{notelist}}

== Reference ==
{{reflist|30em}}

[[Категорија:Ракете]]
[[Категорија:Ракета носач]]
[[Категорија:Ракетна горива]]
[[Категорија:Ракетна погонска горива]]
[[Категорија:Ракетна техника]]
[[Категорија:Ракетни мотори]]
[[Категорија:Свемирска трка]]
[[Категорија:Свемирске летелице]]