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Darkcoucou (talk | contribs) →History: Added Sources and slightly reworded sentences. |
Darkcoucou (talk | contribs) →Table of versions: Filled gaps in the table of engines, particularly Length, Chamber pressure and Expansion Ratio, added reference |
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Line 130:
| 5:1
| 40:1
| {{cvt|20.7|bar}}
| 430 s
| [[Centaur (rocket stage)|Centaur A]]
| Prototype<br /><ref name="Norbert"/><ref name="EA10A1">{{cite encyclopedia |url=http://www.astronautix.com/engines/rl10a1.htm |title=RL-10A-1 |encyclopedia=Encyclopedia Astronautica |first=Mark |last=Wade |access-date=February 27, 2012 |date=November 17, 2011 |url-status=dead |archive-url=https://web.archive.org/web/20111115155200/http://www.astronautix.com/engines/rl10a1.htm |archive-date=November 15, 2011 |df=mdy-all}}</ref><ref name="S2S"/><ref name="GSPAC">{{cite web |url=http://space.skyrocket.de/doc_lau/atlas_centaur.htm |title=Atlas Centaur |publisher=Gunter's Space Page |access-date=February 29, 2012}}</ref>
|-
| RL10A-3C
Line 156:
| {{cvt|296|lb|kg|order=flip}}
| {{cvt|15,000|lbf|kN|order=flip}}
| {{cvt|427
| {{cvt|1.73|m}}
|
| 51:1▼
▲|51:1
| 5:1
| 40:1
| {{cvt|20.7|bar}}
|
| Saturn I [[S-IV|S-IV Stage]]
| <ref name="Norbert"/><ref name=":3" />
|-
| RL10A-4
Line 178:
| 5.5:1
| 84:1
| {{cvt|39.8|bar}}
| 392 s
| [[Centaur (rocket stage)|Centaur IIA]]
| <ref name="Norbert"/><ref name="EA10A4">{{cite encyclopedia |url=http://www.astronautix.com/engines/rl10a4.htm |title=RL-10A-4 |encyclopedia=Encyclopedia Astronautica |first=Mark |last=Wade |access-date=February 27, 2012 |date=November 17, 2011 |url-status=dead |archive-url=https://web.archive.org/web/20111115172045/http://www.astronautix.com/engines/rl10a4.htm |archive-date=November 15, 2011 |df=mdy-all}}</ref>
|-
| RL10A-5
Line 194:
| 6:1
| 4:1
| {{cvt|39.8|bar}}
| 127 s
| [[McDonnell Douglas DC-X|DC-X]]
| <ref name="Norbert"/><ref name="EA10A5">{{cite encyclopedia |url=http://www.astronautix.com/engines/rl10a5.htm |title=RL-10A-5 |encyclopedia=Encyclopedia Astronautica |first=Mark |last=Wade |access-date=February 27, 2012 |date=November 17, 2011 |url-status=dead |archive-url=https://web.archive.org/web/20111115141830/http://www.astronautix.com/engines/rl10a5.htm |archive-date=November 15, 2011 |df=mdy-all}}</ref>
|-
| RL10B-2
Line 221:
| {{cvt|99.1|kN}}
| {{cvt|451|isp}}
| {{cvt|1.78|m}}
| {{cvt|1.53|m}}
| 61:1
|
| 84:1
| {{cvt|42|bar}}
| 740 s
| [[Centaur (rocket stage)|Centaur IIIA]]
| <ref name="Norbert"/><ref name="EA10A41">{{cite encyclopedia |url=http://www.astronautix.com/engines/rl10a41.htm |title=RL-10A-4-1 |encyclopedia=Encyclopedia Astronautica |first=Mark |last=Wade |access-date=February 27, 2012 |date=November 17, 2011 |url-status=dead |archive-url=https://web.archive.org/web/20111117134046/http://www.astronautix.com/engines/rl10a41.htm |archive-date=November 17, 2011 |df=mdy-all}}</ref>
|-
| RL10A-4-2
Line 237:
| {{cvt|99.1|kN}}
| {{cvt|451|isp}}
| {{cvt|1.78|m}}
| {{cvt|1.17|m}}
| 61:1
|
| 84:1
| {{cvt|42|bar}}
| 740 s
| [[Centaur (rocket stage)|Centaur IIIB]]<br />Centaur SEC<br />Centaur DEC
| <ref name="Norbert"/><ref name="EA10A42">{{cite encyclopedia |url=http://www.astronautix.com/engines/rl10a42.htm |title=RL-10A-4-2 |encyclopedia=Encyclopedia Astronautica |first=Mark |last=Wade |access-date=February 27, 2012 |date=November 17, 2011 |url-status=dead |archive-url=https://web.archive.org/web/20120130143126/http://www.astronautix.com/engines/rl10a42.htm |archive-date=January 30, 2012 |df=mdy-all}}</ref><ref name=":0" />
|-
| RL10B-X
Line 303:
| 2.46 m (8 ft 0.7 in)
| 1.57 m (4 ft 9 in)
| 57:1
| 5.5:1
| 155:1
|
|
| Centaur V
| <ref name="Norbert"/><ref name=":1">{{cite web|url=http://rocket.com/sites/default/files/documents/Capabilities/PDFs/RL10_data_sheet.pdf|title=Aerojet Rocketdyne RL10 Propulsion System|date=March 2019|website=Aerojet Rocketdyne}}</ref>
|-
| RL10C-2-1
Line 335:
| 3.15 m (10 ft 4.3 in)
| 1.85 m (6 ft 1 in)
| 48:1
| 5.7:1
| 215:1
|
|
| [[Exploration Upper Stage]]
| <ref name="Norbert"/><ref name=":1" />
|-
| RL10C-5-1
| |||