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Expander cycle
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== Comparison of upper-stage expander-cycle engines == {| class="wikitable" style="text-align:center;" |+ Specifications ! γ ! [[RL10]]B-2 ! [[BE-3U]] ! [[Vinci (rocket engine)|Vinci]] ! [[YF-75D]] ! [[YF-79]] ! [[RD-0146]]D ! [[LE-5B]] ! [[LE-9]] |- ! Country of origin | {{USA}} | {{USA}} | {{FRA}} | {{PRC}} | {{PRC}} | {{RUS}} | {{JPN}} | {{JPN}} |- ! Cycle | Expander | Expander bleed cycle | Expander | Expander | Expander | Expander | Expander bleed cycle, <br />chamber expander | Expander bleed cycle |- ! Thrust, vacuum | 110 kN (25,000 lbf) | 769 kN (173,000 lbf)<ref name="rsuqSn7ifpU">{{cite web |title=New Glenn Completes Second Stage Hotfire! |url=https://www.blueorigin.com/news/new-glenn-completes-second-stage-hotfire|website=BlueOrigin |access-date=1 November 2024}}</ref> | 180 kN (40,000 lbf) | 88.36 kN (19,860 lbf) | 250 kN (56,200 lbf) | 68.6 kN (15,400 lbf) | 137.2 kN (30,840 lbf) | 1471 kN (330,000 lbf)<ref>{{Cite web |last1=Watanabe |first1=Daiki |last2=Manako |first2=Hiroyasu |last3=Onga |first3=Tadaoki |last4=Tamura |first4=Takashi |last5=Ikeda |first5=Kazufumi |last6=Isono |first6=Mitsunori |date=December 2016 |title=Combustion Stability Improvement of LE-9 Engine for Booster Stage of H3 Launch Vehicle |url=https://www.mhi.co.jp/technology/review/pdf/e534/e534028.pdf |access-date=2024-03-13 |website=Mitsubishi Heavy Industries Technical Review}}</ref> |- ! Mixture ratio | 5.88 | | 5.8 | 6.0 | 6.0 | | 5 | 5.9 |- ! Nozzle ratio | 280 | | 240 | 80 | 160 | | 110 | 37 |- ! [[Specific impulse|''I''<sub>sp</sub>]], vacuum (s) | 462<ref>{{Cite web |url=http://www.rocket.com/rl10-engine |title=RL10 Engine | Aerojet Rocketdyne |access-date=2017-06-06 |archive-url=https://web.archive.org/web/20170430183058/http://www.rocket.com/rl10-engine |archive-date=2017-04-30 |url-status=dead }}</ref> | 455<ref>{{Cite web |last=Limp |first=David |date=2024-11-12 |title=The BE-3U's nozzles release hydrogen-rich steam at speeds of roughly 10,000 mph |url=https://x.com/davill/status/1856436665788854463 |access-date=2024-11-29 |website=Twitter}}</ref> | 457 | 442.6 | 455.2 | 470 | 447 | 426 |- ! Chamber pressure (MPa) | 4.412 | | 6.1 | 4.1 | 7.0 | 5.9 | 3.58 | 10.0 |- ! LH<sub>2</sub> TP (rpm) | | | 65,000 | 98,180 | | | 52,000 | |- ! LOX TP (rpm) | | | | | | | 18,000 | |- ! Length (m) | 4.14 | | 4.2 | | | 3.358 | 2.79 | 3.8 |- ! Dry mass (kg) | 277 | | 280 | 265 | | | 285 | 2400 |}
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