Ogled vira Primerjava raketnih motorjev

'''Primerjava raketnih motorjev''', seznam vsebuje [[raketne motor|raketne motorje]] na [[Raketni motor na trdo gorivo|trda]], [[Raketni motor na tekoče gorivo|tekoča goriva]] in [[ionski potisnik|ionske potisnike]]. Seznam ne vsebuje vseh motorjev. 

Okrajšave:
*LOX (Liquid Oxygen) - [[tekoči kisik]]
*LH2 (Liquid Hydrogen) - [[tekoči vodik]]
*RP-1 (Rocket Propellant-1) - [[kerozin]]
*HTPD (Hydroxyl-terminated polybutadiene)
*H2O2 (Hydrogen peroxide) - [[vodikov peroksid]] 
*APCP (Ammonium perchlorate composite propellant)
*N2O4 (Dinitrogen tetroxide) - [[didušikov tetroksid]] 

{|class="wikitable sortable"
! width=120 | Raketni motor
! Država
! Izdelovalec
! Nosilna raketa
! Stopnja
! Gorivo 
! [[Specifični impulz|Specifični impulz (vakuum)]] (s)
! Potisk v vakuumu (N)
! Masa (kg)
! [[Razmerje potisk/teža]]
! Pritisk v zgorevalni komori (bar)
! Status
! width=60|Motor
|- style="background:lightgrey;font-style:italic"
|[[Vulcain]]<ref name="Vulcain">{{navedi splet |url=http://www.astronautix.com/engines/vulcain.htm |title=Vulcain |first= |last= |archiveurl=https://web.archive.org/web/20140805143304/http://astronautix.com/engines/vulcain.htm |archivedate=2014-08-05 |work=Encyclopedia Astronautica |accessdate=27 December 2011 |url-status=bot: unknown }}</ref>
<small>HM-60</small>
|{{Flag|Evropa}}
|[[Aérospatiale]]
|[[Ariane 5]]
| Prva
|[[LH2]]/[[LOX]]
| {{nts|431}}
| {{nts|1075000}}
| {{nts|1300}}
| {{nts|84,318}}
| {{nts|102}}
| Upokojen
|[[Vulcain]]
|- style="background:white;font-style:italic;"
|[[Vulcain|Vulcain 2]]<ref name="Vulcain2">{{navedi splet |url=http://www.astronautix.com/engines/vulcain2.htm |title=Vulcain 2 |first= |last= |archiveurl=https://web.archive.org/web/20141102174242/http://www.astronautix.com/engines/vulcain2.htm |archivedate=2014-11-02 |work=Encyclopedia Astronautica |accessdate=27 December 2011 |url-status=bot: unknown }}</ref><ref name="Vulcain2_Astrium">{{navedi splet |url= http://cs.astrium.eads.net/sp/brochures/launcher-propulsion/Vulcain2.pdf |title= VULCAIN 2 : Thrust Chamber |first=  |last=  |archiveurl= https://web.archive.org/web/20140520155053/http://cs.astrium.eads.net/sp/brochures/launcher-propulsion/Vulcain2.pdf |archivedate= 2014-05-20 |work= astrium.eads.net |accessdate= 27 December 2011 |url-status= dead }}</ref>
|{{Flag|Evropa}}
|[[Aérospatiale]]
|[[Ariane 5]]
| Prva
|[[LH2]]/[[LOX]]
| {{nts|429}}
| {{nts|1359000}}
| {{nts|1800}}
| {{nts|81,04}}?<ref group="Op."><math>\frac{1,340,000\ \mathrm{N}}{(1,686\ \mathrm{kg})(9.807\ \mathrm{m/s^2})}=81.04</math></ref>
| 
| V uporabi
|[[Vulcain|Vulcain 2]]
|- style="background:white;font-style:italic;"
|[[Ariane_5#Solid_boosters|P230]]<ref name="P230">{{navedi splet |url=http://www.astronautix.com/engines/p230.htm |title=P230 |first= |last= |archiveurl=https://web.archive.org/web/20140805132744/http://astronautix.com/engines/p230.htm |archivedate=2014-08-05 |work=Encyclopedia Astronautica |accessdate=27 December 2011 |url-status=bot: unknown }}</ref>
|{{Flag|Evropa}}
|[[Société Nationale des Poudres et Explosifs]] (SNPE)
|[[Ariane 5]]
|Trdogorivni potisnik
|[[HTPB]](68/18)
| {{nts|286}}
| {{nts|6472300}}
| {{nts|268000}} 
| 
|
| V uporabi
|[[Ariane_5#Solid_boosters|P230]]
|- style="background:white;font-style:italic;"
|[[HM7B]]<ref name="Hm7b_Astronautix">{{navedi splet |url=http://www.astronautix.com/engines/hm7b.htm |title=HM7-B |first= |last= |archiveurl=https://web.archive.org/web/20141027085144/http://www.astronautix.com/engines/hm7b.htm |archivedate=2014-10-27 |work=Encyclopedia Astronautica |accessdate=27 April 2012 |url-status=bot: unknown }}</ref><ref name="Hm7b_Snecma">{{navedi splet |url= http://www.snecma.com/IMG/files/fiche_hm7b_2011_modulvoir_file_fr.pdf |title= PROPULSION SPATIALE : HM7B |first=  |last=  |archiveurl= https://web.archive.org/web/20141223170043/http://www.snecma.com/IMG/files/fiche_hm7b_2011_modulvoir_file_fr.pdf |archivedate= 2014-12-23 |work= astrium.eads.net |accessdate= 27 April 2012 |url-status= bot: unknown }}</ref>
|{{Flag|Evropa}}
|[[Snecma]]
|[[Ariane 5|Ariane 5 ECA]]
| Zgornja
|[[LH2]]/[[LOX]]
| {{nts|446}}
| {{nts|64800}}
| {{nts|165}}
| {{nts|40,05}}?<ref group="Op."><math>\frac{64,800\ \mathrm{N}}{(165\ \mathrm{kg})(9.807\ \mathrm{m/s^2})}=40.05</math></ref>
| {{nts|37}}
| V uporabi
|[[HM7B]]
|- style="background:white;font-style:italic"
|[[RD-180]]<ref name="RD-180">{{navedi splet |url= http://www.pw.utc.com/products/pwr/propulsion_solutions/rd-180.asp |title=RD-180}}</ref>
|{{RUS}}
|[[NPO Energomaš]]
|[[Atlas V]]
| Prva
|[[RP-1]]/[[LOX]]
| {{nts|338}}
| {{nts|4150000}}
| {{nts|5480}}
| {{nts|78,44}}
| {{nts|266,8}}
| V uporabi
|[[RD-180]]

|- style="background:white;font-style:italic;"
|[[RD-191]]
|{{RUS}}
|[[NPO Energomaš]]
|[[Angara (Družina raket)]]
| Prva
|[[RP-1]]/[[LOX]]
| {{nts|337}}
| {{nts|2090000}}
| {{nts|2200}}
| {{nts|96,9}}?<ref group="Op."><math>\frac{2,090,000\ \mathrm{N}}{(2,200\ \mathrm{kg})(9.807\ \mathrm{m/s^2})}=96.9</math></ref>
| {{nts|263,4}}
| V uporabi
|[[RD-191]]

|- style="background:white;font-style:italic"
| [[RD-0124]]
<small>14Д23</small>
| {{RUS}}
| [[TsSKB Progress]]
| [[Sojuz (raketa)]]<br>[[Angara (družina raket)]]
| Druga in tretja
| [[RP-1]]/[[LOX]]
| {{nts|359}}
| {{nts|294300}}
| {{nts|480}}
| {{nts|62,5}}?<ref group="Op."><math>\frac{294,300\ \mathrm{N}}{(480\ \mathrm{kg})(9.807\ \mathrm{m/s^2})}=62.5</math></ref>
| {{nts|162}}
| V uporabi
|[[RD-0124]]

|- style="background:white;font-style:italic"
|[[NK-33|NK-33-1 (AJ26-58)]]<ref name="NK33">{{navedi splet |url=http://www.astronautix.com/engines/nk33.htm |title=NK-33 |first= |last= |archiveurl=https://web.archive.org/web/20020625124013/http://www.astronautix.com/engines/nk33.htm |archivedate=2002-06-25 |work=Encyclopedia Astronautica |accessdate=30 January 2014 |url-status=bot: unknown }}</ref>
<small>11Д111</small>
|{{USSR}}
|[[Kuznecov]]<br>[[Aerojet]]
|[[Antares (raketa)]]<br>[[Soju (raketa)]]
| Prva
|[[RP-1]]/[[LOX]]
| {{nts|331}}
| {{nts|1638000}}
| {{nts|1222}}
| {{nts|136,8}}
| {{nts|145}}
| V uporabi
|[[NK-33|NK-33-1 (AJ26-58)]]
|- style="background:lightgrey;font-style:italic"
|[[Bristol Siddeley Gamma|Gamma 8]]<ref name="Gamma8">{{navedi splet |url=http://www.astronautix.com/engines/gamma8.htm |title=Gamma 8 |first= |last= |archiveurl=https://web.archive.org/web/20140805134832/http://astronautix.com/engines/gamma8.htm |archivedate=2014-08-05 |work=Encyclopedia Astronautica |accessdate=26 April 2013 |url-status=bot: unknown }}</ref>
|{{Flag|Združeno kraljestvo}}
|[[Bristol Siddeley]]
|[[Black Arrow]]
| Prva
|[[H2O2]]/[[Kerozin]]
| {{nts|265}}
| {{nts|234800}}
| {{nts|342}}
| {{nts|70,01}}
| {{nts|47,40}}
| Upokojen
|[[Bristol Siddeley Gamma|Gamma 8]]
|- style="background:lightgrey;font-style:italic"
|[[Bristol Siddeley Gamma|Gamma 2]]<ref name="Gamma2">{{navedi splet |url=http://www.astronautix.com/engines/gamma2.htm |title=Gamma 2 |first= |last= |archiveurl=https://web.archive.org/web/20140805134758/http://astronautix.com/engines/gamma2.htm |archivedate=2014-08-05 |work=Encyclopedia Astronautica |accessdate=26 April 2013 |url-status=bot: unknown }}</ref>
|{{Flag|Združeno kraljestvo}}
|[[Bristol Siddeley]]
|[[Black Arrow]]
| Druga
|[[H2O2]]/[[Kerozin]]
| {{nts|265}}
| {{nts|68200}}
| {{nts|173}}
| {{nts|40,22}}
| {{nts|}}
| Upokojen
|[[Bristol Siddeley Gamma|Gamma 2]]
|- style="background:lightgrey;font-style:italic"
|[[Waxwing (Rocket motor)|Waxwing]]<ref name="Waxwing">{{navedi splet |url=http://www.astronautix.com/engines/blarrow3.htm |title=Black Arrow-3 |first= |last= |archiveurl=https://web.archive.org/web/20140805132835/http://astronautix.com/engines/blarrow3.htm |archivedate=2014-08-05 |work=Encyclopedia Astronautica |accessdate=26 April 2013 |url-status=bot: unknown }}</ref>
|{{Flag|Združeno kraljestvo}}
|[[Bristol Aerojet]]
|[[Black Arrow]]
| Zgornja
||Trdogorivni potisnik
| {{nts|278}}
| {{nts|29400}}
| {{nts|87}}
| {{nts|}}
| {{nts|}}
| Upokojen
|[[Waxwing]]
|- style="background:lightgray;font-style:italic;"
|[[Merlin (raketni motor)|Merlin 1C]]
|{{USA}}
|[[SpaceX]]
|[[Falcon 9]]<br>[[Falcon 1]]
| 1/2
|[[RP-1]]/[[LOX]]
| {{nts|304,8}}
| {{nts|480000}}
| {{nts|630}}
| {{nts|96}}
| {{nts|67,7}}
| Upokojen
|[[Merlin (raketni motor)|Merlin 1C]]
|- style="background:white;font-style:italic;"
|[[Merlin (raketni motor)|Merlin 1D]]
<small>Raketni motor z največjim razmerje potsik/teža</small><ref name="smallestTTW">{{navedi novice|url=http://www.spacex.com/press/2013/04/13/spacexs-merlin-1d-engine-achieves-flight-qualification|date=March 20, 2013|publisher=SpaceX|title=Spacex's Merlin 1D Engine Achieves Flight Qualification|accessdate=2014-12-23|archive-date=2014-12-23|archive-url=https://web.archive.org/web/20141223163915/http://www.spacex.com/press/2013/04/13/spacexs-merlin-1d-engine-achieves-flight-qualification|url-status=dead}}</ref>
|{{USA}}
|[[SpaceX]]
|[[Falcon 9]]<br>[[Falcon Heavy]]
| 1/2
|[[RP-1]]/[[LOX]]
| {{nts|310}}
| {{nts|720000}}
| {{nts|490}}
| {{nts|150}}
| {{nts|97}}
| V uporabi
|[[Merlin (raketni motor)|Merlin 1D]]
|- style="background:khaki;font-style:italic;"
|[[Raptor (rocket engine)|Raptor]]<ref name=dn20121213>{{navedi novice |url=http://news.discovery.com/space/alien-life-exoplanets/mars-colony-spacex-121126.htm |title=Huge Mars Colony Eyed by SpaceX Founder |date=2012-12-13 |accessdate=2014-03-14 |publisher=Discovery News |archive-date=2014-11-15 |archive-url=https://web.archive.org/web/20141115083758/http://news.discovery.com/space/alien-life-exoplanets/mars-colony-spacex-121126.htm |url-status=dead }}</ref>
|{{USA}}
|[[SpaceX]]
|
| Prva
|[[Tekoči metan]]/[[LOX]]
| {{nts|380}}
| {{nts|8200000}}<ref name=aw20140609>{{navedi novice |last1=Butler|first1=Amy|last2=Svitak|first2=Amy |title=AR1 vs. Raptor: New rocket program will likely pit kerosene against methane |accessdate=2014-07-07 |issue=2014-06-09 |pp= |publisher=Aviation Week & Space Technology |quote=''SpaceX is developing the Raptor as a reusable engine for a heavy-lift Mars vehicle, the first stage of which will feature 705 metric tons of thrust, making it 'slightly larger than the Apollo F-1 engine,' Tom Mueller, SpaceX vice president of propulsion development, said during a space propulsion conference last month in Cologne, Germany.  The vacuum version is targeting 840 metric tons of thrust with 380 sec. of specific impulse.  The company is testing subscale components using the E-2 test stand at NASA's Stennis Space Center in Mississippi, says Stennis spokeswoman Rebecca Strecker. ... Mueller said many people ask why the company switch to methane for its Mars rocket.  With reusability in mind, SpaceX's cost studies revealed that 'by far the most cost-effective propellant to use is methane,' he said, which would be easier than hydrogen to manufacture on Mars.''}}</ref>
| 
| 
| {{nts|}}
| V razvoju
|[[Raptor (raketni motor)|Raptor]]
|- style="background:white;font-style:italic;"
|[[RD-170|RD-171M]]
<small>Najmočnješi tekočegorivni raketni motor<ref name="RD-171M">{{navedi splet |url=http://www.npoenergomash.ru/eng/engines/rd171m/ |title=RD-171M |first= |last= |archiveurl=https://web.archive.org/web/20140503152712/http://www.npoenergomash.ru/eng/engines/rd171m/ |archivedate=2014-05-03 |work=Encyclopedia Astronautica |accessdate=26 November 2012 |url-status=dead }}</ref></small>
|{{RUS}}
|[[NPO Energomaš]]
|[[Zenit-3SL]] ([[Sea Launch]])<br>[[Zenit-3SLB]] ([[Land Launch]])
| Prva
|[[RP-1]]/[[LOX]]
| {{nts|337,2}}
| {{nts|7904000}}
| {{nts|9300}}
| {{nts|86,6}}
| 
| V uporabi
|[[RD-170|RD-171M]]
|- style="background:white;font-style:italic;"
|[[RD-107|RD-107A]]<ref name="npo_107_108">{{navedi splet |url=http://www.npoenergomash.ru/engines/rd107/rd107_1.html |title=РД-107/108 |first= |last= |archiveurl=https://web.archive.org/web/20140224194031/http://www.npoenergomash.ru/engines/rd107/rd107_1.html |archivedate=2014-02-24 |work=NPO Energomash |accessdate=27 November 2012 |url-status=dead }}</ref>
<small>14Д22</small>
|{{RUS}}
|[[NPO Energomaš]]
|[[Sojuz-FG]]<br>[[Sojuz-2]]
| Prva
|[[RP-1]]/[[LOX]]
| {{nts|320,2}}
| {{nts|1020240}}
| {{nts|1156}}
| {{nts|}}
| {{nts|61,2}}
| V uporabi
|[[RD-107|RD-107A]]
|- style="background:white;font-style:italic;"
|[[RD-107|RD-108A]]
<small>14Д21</small>
|{{RUS}}
|[[NPO Energomaš]]
|[[Sojuz-FG]]<br>[[Sojuz-2]]
| Druga
|[[RP-1]]/[[LOX]]
| {{nts|320,6}}
| {{nts|922140}}
| {{nts|1151}}
| {{nts|}}
| {{nts|55,5}}
| V uporabi
|[[RD-107|RD-108A]]
|- style="background:white;font-style:italic;"
|[[RD-107|RD-117]]<ref name="lpre">{{navedi splet |url=http://www.lpre.de/energomash/RD-107/index.htm |title=RD-117 |first= |last= |archiveurl=https://web.archive.org/web/20150213024157/http://lpre.de/energomash/RD-107/index.htm |archivedate=2015-02-13 |work=lpre.de |accessdate=27 November 2012 |url-status=bot: unknown }}</ref>
<small>11Д511</small>
|{{USSR}}
|[[NPO Energomaš]]
|[[Sojuz-U]]
| Prva
|[[RP-1]]/[[LOX]]
| {{nts|315,8}}
| {{nts|978000}}
| {{nts|1250}}
| {{nts|}}
| {{nts|53,2}}
| V uporabi
|[[RD-107|RD-117]]
|- style="background:white;font-style:italic;"
|[[RD-107|RD-118]]
<small>11Д512</small>
|{{USSR}}
|[[NPO Energomaš]]
|[[Sojuz-U]]
| Druga
|[[RP-1]]/[[LOX]]
| {{nts|314,5}}
| {{nts|999639}}
| {{nts|1155}}
| {{nts|}}
| {{nts|58,6}}
| V uporabi
|[[RD-107|RD-118]]
|- style="background:lightgrey;font-style:italic"
|[[LE-5]]
|{{JPN}}
|[[Mitsubishi Heavy Industries]]<br>[[National Space Development Agency of Japan|NASDA]]
|[[H-I]]
| Zgornja
|[[LH2]]/[[LOX]]
| {{nts|450}}
| {{nts|102900}}
| {{nts|255}}
| {{nts|}}
| {{nts|36,5}}
| Upokojen
|[[LE-5]]
|- style="background:lightgrey;font-style:italic"
|[[LE-5|LE-5A]]
|{{JPN}}
|[[Mitsubishi Heavy Industries]]<br>[[National Space Development Agency of Japan|NASDA]]
|[[H-II]]
| Zgornja
|[[LH2]]/[[LOX]]
| {{nts|452}}
| {{nts|121500}}
| {{nts|248}}
| {{nts|}}
| {{nts|39,8}}
| Upokojen
|[[LE-5|LE-5A]]
|- style="background:white;font-style:italic;"
|[[LE-5|LE-5B]]
|{{JPN}}
|[[Mitsubishi Heavy Industries]]<br>[[Japan Aerospace Exploration Agency|JAXA]]
|[[H-IIA]]<br/>[[H-IIB]]
| Zgornja
|[[LH2]]/[[LOX]]
| {{nts|447}}
| {{nts|137200}}
| {{nts|285}}
| {{nts|49,1}}?<ref group="Op."><math>\frac{137,200\ \mathrm{N}}{(285\ \mathrm{kg})(9.807\ \mathrm{m/s^2})}=49.1</math></ref>
| {{nts|35,8}}
| V uporabi
|[[LE-5|LE-5B]]
|- style="background:lightgrey;font-style:italic"
|[[LE-7]]
|{{JPN}}
|[[Mitsubishi Heavy Industries]]<br>[[National Space Development Agency of Japan|NASDA]]
|[[H-II]]
| Prva
|[[LH2]]/[[LOX]]
| {{nts|446}}
| {{nts|1078000}}
| {{nts|1714}}
| {{nts|64,13}}
| {{nts|127}}
| Upokojen
|[[LE-7]]
|- style="background:white;font-style:italic;"
|[[LE-7|LE-7A]]
|{{JPN}}
|[[Mitsubishi Heavy Industries]]<br>[[Japan Aerospace Exploration Agency|JAXA]]
|[[H-IIA]]<br/>[[H-IIB]]
| Prva
|[[LH2]]/[[LOX]]
| {{nts|440}}
| {{nts|1098000}}
| {{nts|1800}}
| {{nts|65,9}}
| {{nts|120}}
| V uporabi
|[[LE-7|LE-7A]]
|- style="background:white;font-style:italic;"
|[[SRB-A]]
|{{JPN}}
|[[IHI Corporation|IHI Aerospace]]<br>[[Japan Aerospace Exploration Agency|JAXA]]
|[[H-IIA]]<br/>[[H-IIB]]
| Trdogorivni potisnik
| Trdo
| {{nts|280}} (SRB-A)<br/>{{nts|284}} (SRB-A3 verzija H-IIA F18)
| {{nts|2260000}} (SRB-A)<br/>{{nts|2500000}} (SRB-A3 verzija H-IIA F18)
| {{nts|71800}} 
| {{nts|}}
| {{nts|}}
| V uporabi
|[[SRB-A]]
|- style="background:white;font-style:italic;"
|[[RS-68A]]
<small>Najmočnejši raketni motor na vodik</small>
|{{USA}}
|[[Pratt & Whitney Rocketdyne]]
|[[Delta IV]]<br>[[Delta IV Heavy]]
| Prva
|[[LH2]]/[[LOX]]
| {{nts|412}}
| {{nts|3560000}}<ref>{{navedi splet|title=Delta IV Heavy|url=http://www.spaceflight101.com/delta-iv-heavy.html|work=SPACEFLIGHT101|accessdate=2 November 2014|ref=RS-68A|archive-date=2014-12-13|archive-url=https://web.archive.org/web/20141213231645/http://www.spaceflight101.com/delta-iv-heavy.html|url-status=dead}}</ref>
| {{nts|6600}}
| {{nts|51,2}}
| {{nts|97}}
| V uporabi
|[[RS-68A]]
|- style="background:white;font-style:italic;"
|[[Atlas V|Atlas V SRB]]
|{{USA}}
|[[Aerojet]]
|[[Atlas V]]
|[[Trdogorivni potisnik]]
|Trdo
| 
|
| {{nts|40824}} z gorivom
| 
| 
| V uporabi
|[[Atlas V|Atlas V SRB]]
|- style="background:lightgrey;font-style:italic;"
|[[F-1 (raketni motor)]]
<small>Najmočnejši tekočegorivni motor z eno šobo</small>
|{{USA}}
|[[Rocketdyne]]
|[[Saturn V]]
| Prva
|[[RP-1]]/[[LOX]]
| {{nts|263}}
| {{nts|6770000}}
| {{nts|8391}}
| {{nts|82,27}}?<ref group="Op."><math>\frac{6,770,000\ \mathrm{N}}{(8,391\ \mathrm{kg})(9.807\ \mathrm{m/s^2})}=82.27</math></ref>
| {{nts|70}}
| Upokojen
|[[F-1 (raketni motor)|F-1]]
|- style="background:white;font-style:italic;"
|[[RS-25 - SSME]]
|{{USA}}
|[[Pratt & Whitney Rocketdyne]]
|[[Space shuttle]]
| Prva
|[[LH2]]/[[LOX]]
| {{nts|452,3}}
| {{nts|2279000}}
| {{nts|3526}}
| {{nts|65,91}}?<ref group="Op."><math>\frac{2,279,000\ \mathrm{N}}{(3,526\ \mathrm{kg})(9.807\ \mathrm{m/s^2})}=65.91</math></ref>
| {{nts|206,4}}
| Upokojen
|[[Space Shuttle Main Engine|RS-25]]
|- style="background:white;font-style:italic;"
|[[Space Shuttlov trdogorivni potisnik]]
<small>Najmočnejši raketni motor, ki je poletel</small>
|{{USA}}
|[[Thiokol]]
|[[Space Shuttle]]<br>[[Ares I]]
|Trdogorivni potisnik
|[[APCP]]
| {{nts|268}}
| {{nts|14000000}}
| {{nts|590000}}<br>z gorivom
| 
| 
| Neaktiven
|[[Space Shuttlov trdogorivni potisnik]]
|- style="background:lightgrey;font-style:italic;"
|[[J-2 (rocket engine)|J-2]]<ref name="J-2">{{navedi splet |url=http://www.astronautix.com/engines/j2.htm |title=J-2 |first= |last= |archiveurl=https://web.archive.org/web/20150202013539/http://astronautix.com/engines/j2.htm |archivedate=2015-02-02 |work=Encyclopedia Astronautica |accessdate=23 December 2011 |url-status=bot: unknown }}</ref>
|{{USA}}
|[[Rocketdyne]]
|[[Saturn V]]<br>[[Saturn IB]]
| Prva
|[[LH2]]/[[LOX]]
| {{nts|421}}
| {{nts|1033100}}
| {{nts|1438}}
| {{nts|73,18}}
| {{nts|30}}
| Upokojen
|[[J-2]]
|- style="background:khaki;font-style:italic;"
|[[J-2X]]<ref name="J-2X">{{navedi splet |url=http://www.pw.utc.com/products/pwr/propulsion_solutions/j-2x.asp |title=J-2X Engine |first= |last= |archiveurl=https://web.archive.org/web/20120624064512/http://www.pw.utc.com/products/pwr/propulsion_solutions/j-2x.asp |archivedate=2012-06-24 |work=Pratt & Whitney Rocketdyne |accessdate=23 December 2011 |url-status=bot: unknown }}</ref><ref name="J-2X-2">{{navedi splet |url=http://www.astronautix.com/engines/j2x.htm |title=J-2X |first= |last= |archiveurl=https://web.archive.org/web/20140805144229/http://astronautix.com/engines/j2x.htm |archivedate=2014-08-05 |work=Encyclopedia Astronautica |accessdate=23 December 2011 |url-status=bot: unknown }}</ref>
|{{USA}}
|[[Pratt & Whitney Rocketdyne]]
|[[Space Launch System]]
| Zgornja
|[[LH2]]/[[LOX]]
| {{nts|448}}
| {{nts|1310000}}
| {{nts|2430}}
| {{nts|54,97}}?<ref group="Op."><math>\frac{1,310,000\ \mathrm{N}}{(2,430\ \mathrm{kg})(9.807\ \mathrm{m/s^2})}=54.97</math></ref>
| {{nts|30}}
| V razvoju
|[[J-2X]]
|- style="background:white;font-style:italic;"
|[[RL10|RL-10B-2]]<ref name="RL-10B-2">{{navedi splet |url=http://www.astronautix.com/engines/rl10b2.htm |title=RL-10B-2 |first= |last= |archiveurl=https://web.archive.org/web/20141204164912/http://www.astronautix.com/engines/rl10b2.htm |archivedate=2014-12-04 |work=Encyclopedia Astronautica |date=23 December 2011 |accessdate=2014-12-23 |url-status=bot: unknown }}</ref><ref name="RL-10">{{navedi splet |url=http://www.spaceandtech.com/spacedata/engines/rl10_specs.shtml |title=RL-10 - Specifications |first= |last= |archiveurl=https://web.archive.org/web/20111201181248/http://www.spaceandtech.com/spacedata/engines/rl10_specs.shtml |archivedate=2011-12-01 |work=Spaceandtech |date=23 December 2011 |accessdate=2014-12-23 |url-status=bot: unknown }}</ref>
|{{USA}}
|[[Pratt & Whitney Rocketdyne]]
|[[Delta III]]<br>[[Delta IV]]
| Zgornja
|[[LH2]]/[[LOX]]
| {{nts|462}}
| {{nts|109890}}
| {{nts|277}}
| {{nts|41}}
| {{nts|44}}
| V uporabi
|[[RL10|RL-10B-2]]
|- style="background:white;font-style:italic;"
|[[RL10|RL-10A-4-2]]<ref name="RL-10"/><ref name="RL-10A-4-2">{{navedi splet |url=http://www.astronautix.com/engines/rl10a42.htm |title=RL-10A-4-2 |first= |last= |archiveurl=https://web.archive.org/web/20140805141545/http://astronautix.com/engines/rl10a42.htm |archivedate=2014-08-05 |work=Encyclopedia Astronautica |date=23 December 2011 |accessdate=2014-12-23 |url-status=bot: unknown }}</ref>
|{{USA}}
|[[Pratt & Whitney Rocketdyne]]
|[[Atlas V]]
| Zgornja
|[[LH2]]/[[LOX]]
| {{nts|451}}
| {{nts|99100}}
| {{nts|167}}
| {{nts|59}}
| {{nts|39}}
| V uporabi
|[[RL10|RL-10A-4-2]]
|- style="background:white;font-style:italic;"
|[[NSTAR ion engine|NSTAR]]<ref name="NSTAR">{{cite journal|url=http://www.grc.nasa.gov/WWW/ion/past/90s/nstar.htm|author1=Sovey, J.S.|author2=Rawlin, V.K.|author3=Patterson, M.J.|title=Ion Propulsion Development Projects in U. S.: Space Electric Rocket Test 1 to Deep Space 1.|work=Journal of Propulsion and Power|volume=17|issue=3|date=May–June 2001|pages=517–526.|access-date=2014-12-23|archive-date=2015-03-20|archive-url=https://web.archive.org/web/20150320054002/http://www.grc.nasa.gov/WWW/ion/past/90s/nstar.htm|url-status=dead}}</ref><ref name="NSTAR_boeing">{{navedi splet |url= http://www.boeing.com/defense-space/space/bss/factsheets/xips/nstar/ionengine.html |title= Hughes' Ion Engine Serving as Primary Propulsion to NASA's Deep Space 1 |first=  |last=  |archiveurl= https://web.archive.org/web/20120716204407/http://www.boeing.com/defense-space/space/bss/factsheets/xips/nstar/ionengine.html |archivedate= 2012-07-16 |work= www.boeing.com |date= 24 December 2011 |accessdate= 2014-12-23 |url-status= bot: unknown }}</ref>
|{{USA}}
|[[Hughes Electron Dynamics]]<br>[[Boeing]]
|[[Deep Space 1]]<br>[[Dawn (spacecraft)|Dawn]]
|[[Ionski potisnik]]
|[[Ksenon]]
| {{nts|3100}} @2,3&nbsp;kW
| {{nts|0,0920}} @2,3&nbsp;kW
| {{nts|8,2}}
| 
| 
| V uporabi
|[[NSTAR ionski potisnik|NSTAR]]
|- style="background:lightgrey;font-style:italic;"
|[[HiPEP]]
<small>Najmočnejši ionski potisnik</small>
|{{USA}}
|[[NASA]]
|[[Jupiter Icy Moons Orbiter]]
|[[Ionski potisnik]]
|[[Ksenon]]
| {{nts|9620}} @39,3&nbsp;kW
| {{nts|0,670}} @39,3&nbsp;kW
| 
| 
| 
| Preklican
|[[HiPEP]]
|- style="background:khaki;font-style:italic;"
|[[NEXT (ion thruster)|NEXT]]
|{{USA}}
|[[NASA]]
|
|[[Ionski potisnik]]
|[[Ksenon]]
| {{nts|4100}} @6,9&nbsp;kW
| {{nts|0,236}} @6,9&nbsp;kW
| 
| 
| 
| V razvoju
|[[NEXT (ionski potisnik)|NEXT]]
|- style="background:khaki;font-style:italic;"
|[[VASIMR]]
|{{USA}}
|[[Ad Astra Rocket Company]]
|
| [[Elektromagnetni potisnik]]
| [[Argon]]
| {{nts|5000}} @200&nbsp;kW
| {{nts|5}}? @200&nbsp;kW
| 
| 
| 
| V razvoju
|[[VASIMR]]
|- style="background:white;font-style:italic;"
|[[PPS-1350]]
|{{RUS}}<br>{{Flag|Evropa}}
|[[OKB Fakel]]<br>[[Snecma]]
| [[SMART-1]]
| [[Hall potisnik]]
| [[Ksenon]]
| {{nts|1650}} @1,5&nbsp;kW
| {{nts|0.088}} @1,5&nbsp;kW
| {{nts|5,3}}
| {{nts|0,0017}}?<ref group="Op."><math>\frac{0.088\ \mathrm{N}}{(5.3\ \mathrm{kg})(9.807\ \mathrm{m/s^2})}=0.0017</math></ref>
| 
| V uporabi
|[[PPS-1350]]
|- style="background:white;font-style:italic;"
|[[SPT-100]]
|{{RUS}}
|[[OKB Fakel]]
| [[LS-1300]] sateliti
| [[Hall potisnik]]
| [[Ksenon]]
| {{nts|1500}} @1,35&nbsp;kW
| {{nts|0,083}} @1,35&nbsp;kW
| {{nts|3,5}}
| {{nts|0,0024}}?<ref group="Op."><math>\frac{0.083\ \mathrm{N}}{(3.5\ \mathrm{kg})(9.807\ \mathrm{m/s^2})}=0.0024</math></ref>
| 
| V uporabi
|[[SPT-100]]
|- style="background:white;font-style:italic;"
|[[Boeing 601HP]]
<small>Prvi ionski potisnik na operativnem komercialnem satelitu ([[PanAmSat|PAS-5]])</small>
|{{USA}}
|[[Boeing]]
|[[Boeing 601HP]] sateliti
| [[Ion thruster]]
| [[Ksenon]]
| {{nts|2568}} @0,5&nbsp;kW
| {{nts|0,018}} @0,5&nbsp;kW
| 
| 
| 
| V uporabi
|[[Boeing 601HP]]
|- style="background:white;font-style:italic;"
|[[Boeing 702]]
|{{USA}}
|[[Boeing]]
|[[Boeing 702]] sateliti
| [[Ionski potisnik]]
| [[Ksenon]]
| {{nts|3800}} @4,5&nbsp;kW
| {{nts|0,165}} @4,5&nbsp;kW
| 
| 
| 
| V uporabi
|[[Boeing 702]]
|- style="background:white;font-style:italic"
|[[KVD-1]]<ref name="KVD1">{{navedi splet|url=http://kbhmisaeva.ru/main.php?id=54|script-title=ru:Двигатель КВД1|publisher=КБХМ им. A.M. Исаева|language=ru|accessdate=2014-12-23|archive-date=2014-02-02|archive-url=https://web.archive.org/web/20140202120044/http://kbhmisaeva.ru/main.php?id=54|url-status=dead}}</ref>
<small>11Д56У</small>
|{{RUS}}
|[[KBKhM]]
|[[GSLV#GSLV_Mk_I_(a)|GSLV Mk I]]
| Zgornja
|[[LH2]]/[[LOX]]
| {{nts|462}}
| {{nts|69626}}
| {{nts|282}}
| {{nts|25,17}}
| {{nts|55,9}}
| Neaktiven
|[[KVD-1]]
|- style="background:white;font-style:italic;"
|[[CE-7.5]]<ref name="CUS">{{navedi splet | url=http://www.isro.gov.in/gslv-d5/cryogenic-engine.aspx | title=Indigenous Cryogenic Engine and Stage | accessdate=6 January 2014 | archive-date=2014-08-06 | archive-url=https://web.archive.org/web/20140806173146/http://isro.gov.in/gslv-d5/cryogenic-engine.aspx | url-status=dead }}</ref><ref name="CE7.5">{{navedi splet | url=http://www.spaceflight101.com/gslv-launch-vehicle-information.html | title=GSLV Launch Vehicle Information | accessdate=6 January 2014 | archive-date=2014-01-06 | archive-url=https://web.archive.org/web/20140106133259/http://www.spaceflight101.com/gslv-launch-vehicle-information.html | url-status=dead }}</ref>
|{{Flag|Indija}}
|[[ISRO]]
|[[GSLV#GSLV_Mk_II|GSLV Mk II]] 
| Upper
| [[LH2]]/[[LOX]]
| {{nts|454}}
| {{nts|73550}}
| {{nts|445}}
| {{nts|16,85}}<ref group="Op."><math>\frac{73,550\ \mathrm{N}}{(445\ \mathrm{kg})(9.807\ \mathrm{m/s^2})}=16.85</math></ref>
| {{nts|58}}
| V uporabi
|[[CE-7.5]]
|- style="background:white;font-style:italic;"
|[[Polar Satellite Launch Vehicle|PSLV-1]]<ref name="PSLV-1">{{navedi splet | url=http://www.astronautix.com/engines/pslv1.htm | title=PSLV-1 | accessdate=4 April 2014}}</ref>
|{{Flag|Indija}}
|[[ISRO]]
|[[PSLV]] 
| Prva
| [[HTPB]]
| {{nts|269}}
| {{nts|4860000}}
| {{nts|160200}}
| 
| {{nts|58}}
| V uporabi
|[[Polar Satellite Launch Vehicle|PSLV-1]]
|- style="background:white;font-style:italic;"
|[[SLV-1]]<ref name="SLV-1">{{navedi splet | url=http://www.astronautix.com/engines/slv1.htm| title=SLV-1 | accessdate=4 April 2014}}</ref>
|{{Flag|Indija}}
|[[ISRO]]
|[[PSLV]] 
| Potisnik
| [[HTPB]]
| {{nts|253}}
| {{nts|502600}}
| {{nts|10800}}
| 
| {{nts|43}}
| V uporabi
|[[SLV-1]]
|- style="background:white;font-style:italic;"
|[[RD-264]]<ref name="RD-264">{{navedi splet | url=http://www.astronautix.com/engines/rd264.htm| title=RD-264 | accessdate=4 April 2014}}</ref>
<small>11Д119</small>
|{{USSR}}
|[[NPO Energomaš]]
|[[Dnepr-1]] 
| Prva
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]/[[UDMH]]
| {{nts|318}}
| {{nts|4521000}}
| {{nts|3600}}
| {{nts|128}}
| {{nts|206}}
| V uporabi
|[[RD-264]]
|- style="background:white;font-style:italic;"
|[[RD-276]]<ref name="RD-276">{{navedi splet| url=http://www.npoenergomash.ru/engines/rd253/| title=РД-253| accessdate=5 April 2014| archive-date=2012-01-10| archive-url=https://web.archive.org/web/20120110173710/http://www.npoenergomash.ru/engines/rd253/| url-status=dead}}</ref>
<small>14Д14М</small>
|{{RUS}}
|[[NPO Energomaš]]
|[[Proton-M]] 
| Prva
| [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]/[[UDMH]]
| {{nts|316}}
| {{nts|1830000}}
| {{nts|1,260}}
| {{nts|148}}
| {{nts|169}}
| V uporabi
|[[RD-276]]
|- style="background:lightgrey;font-style:italic"
|[[RD-0120]]<ref name="RD-0120">{{navedi splet |url=http://www.kbkha.ru/?p=8&cat=8&prod=34 |title= RD0120 |publisher=KBKhA}}</ref>
<small>11Д122</small>
|{{USSR}}
|[[KBKhA]]
|[[Energija]]
| Prva
|[[LH2]]/[[LOX]]
| {{nts|455}}
| {{nts|1962000}}
| {{nts|3450}}
| {{nts|57.80}}
| {{nts|219}}
| Upokojen
|[[RD-0120]]
|- style="background:khaki;font-style:italic;"
|[[RD-193]] (RD-181)<ref name="RD-193">{{navedi splet |url=http://www.parabolicarc.com/2012/10/25/energomash-test-fires-new-rd-193-engine/ |title=Energomash Test Fires New RD-193 Engine |publisher=parabolicarc.com |accessdate=2014-12-23 |archive-date=2014-12-23 |archive-url=https://web.archive.org/web/20141223091124/http://www.parabolicarc.com/2012/10/25/energomash-test-fires-new-rd-193-engine/ |url-status=dead }}</ref>
|{{RUS}}
||[[NPO Energomaš]]
|[[Sojuz-1]]<br>[[Antares (raketa)]]
| Prva
|[[RP-1]]/[[LOX]]
| {{nts|337,5}}
| {{nts|2090000}}>
| {{nts|1900}}
| {{nts|112}}
| 
| V razvoju
|[[RD-193]]
|- style="background:white;font-style:italic;"
|[[Aestus]]<ref name="Aestus_Airbus">{{navedi splet |url= http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/aestus-rocket-engine.html |title= Aestus Rocket Engine |first=  |last=  |archiveurl= https://web.archive.org/web/20141216234911/http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/aestus-rocket-engine.html |archivedate= 2014-12-16 |work= Airbus Defence and Space |accessdate= 29 January 2014 |url-status= bot: unknown }}</ref>
|{{Flag|Evropa}}
|[[Airbus Defence and Space]]
|[[Ariane 5|Ariane 5 ES]]
| Zgornja
|[[N2O4]]/[[MMH]]
| {{nts|324}}
| {{nts|30000}}
| {{nts|111}}
| {{nts|27,6}}
| {{nts|11}}
| V uporabi
|[[Aestus]]
|- style="background:khaki;font-style:italic;"
|[[Aestus II]]<ref name="AestusII_Airbus">{{navedi splet |url= http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/aestus-rs72-rocket-engine.html |title= Aestus Rocket Engine |first=  |last=  |archiveurl= https://web.archive.org/web/20141215222250/http://cs.astrium.eads.net/sp/launcher-propulsion/rocket-engines/aestus-rs72-rocket-engine.html |archivedate= 2014-12-15 |work= Airbus Defence and Space |accessdate= 29 January 2014 |url-status= bot: unknown }}</ref>
|{{Flag|Evropa}}
|[[Airbus Defence and Space]]
|
| Zgornja
|[[N2O4]]/[[MMH]]
| {{nts|340}}
| {{nts|55400}}
| {{nts|138}}
| {{nts|40,9}}
| {{nts|60}}
| V razvoju
|[[Aestus II]]
|- style="background:khaki;font-style:italic;"
|[[Blue Origin]] [[BE-4]]
|{{USA}}
|[[Blue Origin]]
|[[Atlas V]]
| Prva
|[[Tekoči metan]]/[[LOX]]
|ni znano
|
|
|
|
|V razvoju
|[[BE-4]]
|}

== Opombe ==
{{sklici|group=Op.}}

== Sklici ==
{{Reflist|2}}

==Glej tudi==
*[[Primerjava nosilnih raket]]
*[[Primerjava vesoljskih plovil]]

{{Raketni motorji}}
[[Kategorija:Raketni motorji]]