JP2015507719A5 - - Google Patents

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Publication number
JP2015507719A5
JP2015507719A5 JP2014552676A JP2014552676A JP2015507719A5 JP 2015507719 A5 JP2015507719 A5 JP 2015507719A5 JP 2014552676 A JP2014552676 A JP 2014552676A JP 2014552676 A JP2014552676 A JP 2014552676A JP 2015507719 A5 JP2015507719 A5 JP 2015507719A5
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JP
Japan
Prior art keywords
fluid
pump
jet pump
supply pipe
engine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2014552676A
Other languages
English (en)
Japanese (ja)
Other versions
JP6028043B2 (ja
JP2015507719A (ja
Filing date
Publication date
Priority claimed from FR1250460A external-priority patent/FR2985804B1/fr
Application filed filed Critical
Publication of JP2015507719A publication Critical patent/JP2015507719A/ja
Publication of JP2015507719A5 publication Critical patent/JP2015507719A5/ja
Application granted granted Critical
Publication of JP6028043B2 publication Critical patent/JP6028043B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2014552676A 2012-01-17 2013-01-16 燃料供給が最適化されたロケットエンジン Expired - Fee Related JP6028043B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1250460A FR2985804B1 (fr) 2012-01-17 2012-01-17 Moteur pour fusee a alimentation optimisee
FR1250460 2012-01-17
PCT/FR2013/050094 WO2013107981A1 (fr) 2012-01-17 2013-01-16 Moteur pour fusée a alimentation optimisée

Publications (3)

Publication Number Publication Date
JP2015507719A JP2015507719A (ja) 2015-03-12
JP2015507719A5 true JP2015507719A5 (enExample) 2016-02-12
JP6028043B2 JP6028043B2 (ja) 2016-11-16

Family

ID=47714399

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014552676A Expired - Fee Related JP6028043B2 (ja) 2012-01-17 2013-01-16 燃料供給が最適化されたロケットエンジン

Country Status (6)

Country Link
US (1) US20140373507A1 (enExample)
EP (1) EP2805039B1 (enExample)
JP (1) JP6028043B2 (enExample)
FR (1) FR2985804B1 (enExample)
RU (1) RU2014130193A (enExample)
WO (1) WO2013107981A1 (enExample)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111622864B (zh) * 2020-06-03 2023-02-21 陕西天回航天技术有限公司 一种半开式富氧补燃循环发动机
US11945606B1 (en) 2021-10-19 2024-04-02 Ball Aerospace & Technologies Corp. Electric propulsion based spacecraft propulsion systems and methods utilizing multiple propellants
CN115095396B (zh) * 2022-06-24 2024-10-29 西安航天动力研究所 一种液体火箭发动机涡轮出口导流弯管结构

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1626055B1 (de) * 1967-04-05 1970-07-30 Messerschmitt Boelkow Blohm Aus mehreren Flüssigkeitsraketen bestehendes Antriebsaggregat
DE1776010A1 (de) * 1968-09-03 1971-09-16 Messerschmitt Boelkow Blohm Verfahren zum Foerdern von fluessigen Treibstoffen fuer Gaserzeuger bzw.Raketenbrennkammern,und Foerdersystem zur Durchfuehrung des Verfahrens
US5444973A (en) * 1993-12-13 1995-08-29 United Technologies Corporation Pressure-fed rocket booster system
US5551230A (en) * 1994-03-14 1996-09-03 Rockwell International Corporation Heat induced high pressure lox pump rocket engine cycle
RU2158839C2 (ru) * 1999-01-21 2000-11-10 Открытое акционерное общество "НПО Энергомаш им. акад. В.П. Глушко" Жидкостный ракетный двигатель с дожиганием турбогаза
DE19958310C2 (de) * 1999-12-03 2002-01-17 Daimler Chrysler Ag Raketentriebwerk für Flüssigtreibstoffe mit einem geschlossenen Triebwerkskreislauf
JP2002054505A (ja) * 2000-08-11 2002-02-20 Mitsubishi Heavy Ind Ltd ロケットエンジン
US6550253B2 (en) * 2001-09-12 2003-04-22 General Electric Company Apparatus and methods for controlling flow in turbomachinery
US7389636B2 (en) * 2005-07-06 2008-06-24 United Technologies Corporation Booster rocket engine using gaseous hydrocarbon in catalytically enhanced gas generator cycle
US7784268B1 (en) * 2006-08-04 2010-08-31 Xcor Aerospace Partial superheat cycle for operating a pump in a rocket system
US8613189B1 (en) * 2009-11-30 2013-12-24 Florida Turbine Technologies, Inc. Centrifugal impeller for a rocket engine having high and low pressure outlets

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