DE60211774D1 - Cryotechnische Schubeinheit - Google Patents

Cryotechnische Schubeinheit

Info

Publication number
DE60211774D1
DE60211774D1 DE60211774T DE60211774T DE60211774D1 DE 60211774 D1 DE60211774 D1 DE 60211774D1 DE 60211774 T DE60211774 T DE 60211774T DE 60211774 T DE60211774 T DE 60211774T DE 60211774 D1 DE60211774 D1 DE 60211774D1
Authority
DE
Germany
Prior art keywords
cryotechnical
push unit
push
unit
cryotechnical push
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.)
Expired - Lifetime
Application number
DE60211774T
Other languages
English (en)
Other versions
DE60211774T2 (de
Inventor
Dominique Valentian
Jacques Borromee
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SNECMA SAS filed Critical SNECMA SAS
Publication of DE60211774D1 publication Critical patent/DE60211774D1/de
Application granted granted Critical
Publication of DE60211774T2 publication Critical patent/DE60211774T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/94—Re-ignitable or restartable rocket- engine plants; Intermittently operated rocket-engine plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/401—Liquid propellant rocket engines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/402—Propellant tanks; Feeding propellants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/242—Orbits and trajectories
    • B64G1/2427—Transfer orbits
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • B64G1/446—Thermal solar power generation
DE60211774T 2001-03-16 2002-03-14 Cryotechnische Schubeinheit Expired - Lifetime DE60211774T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0103589A FR2822193B1 (fr) 2001-03-16 2001-03-16 Module de propulsion cryotechnique a faible poussee
FR0103589 2001-03-16

Publications (2)

Publication Number Publication Date
DE60211774D1 true DE60211774D1 (de) 2006-07-06
DE60211774T2 DE60211774T2 (de) 2007-05-24

Family

ID=8861208

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60211774T Expired - Lifetime DE60211774T2 (de) 2001-03-16 2002-03-14 Cryotechnische Schubeinheit

Country Status (5)

Country Link
US (1) US6581882B2 (de)
EP (1) EP1241341B1 (de)
DE (1) DE60211774T2 (de)
FR (1) FR2822193B1 (de)
RU (1) RU2282744C2 (de)

Families Citing this family (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6892525B2 (en) * 2003-06-06 2005-05-17 Honeywell International Inc. Micropump-based microthruster
US7273352B2 (en) * 2004-01-09 2007-09-25 United Technologies Corporation Inlet partial blades for structural integrity and performance
US7762498B1 (en) * 2005-06-09 2010-07-27 Lockheed Martin Corporation Enhanced high-efficiency spacecraft propulsion system
US7900434B2 (en) * 2006-12-20 2011-03-08 The Boeing Company Thermally-integrated fluid storage and pressurization system
FR2916485B1 (fr) * 2007-05-24 2011-03-18 Centre Nat Etd Spatiales "dispositif cryotechnique de propulsion dans l'espace et son procede de commande"
GB2484114A (en) * 2010-09-30 2012-04-04 Astrium Ltd System for the Recovery, Storage and Utilisation of Atmospheric Gas for Use as a Vehicle Propellant
RU2447001C1 (ru) * 2010-10-01 2012-04-10 Открытое акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" Устройство для заправки баков космического аппарата топливом методом вытеснения
FR2975441B1 (fr) * 2011-05-16 2016-02-12 Snecma Dispositif et procede de re-pressurisation
RU2474520C1 (ru) * 2011-05-27 2013-02-10 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Двигательная установка ракетного блока
FR2976626B1 (fr) * 2011-06-17 2013-07-05 Snecma Ensemble propulsif cryogenique
US20130043352A1 (en) * 2011-08-18 2013-02-21 Patrick R.E. Bahn Throttleable propulsion launch escape systems and devices
RU2476706C1 (ru) * 2011-09-21 2013-02-27 Николай Борисович Болотин Жидкостный ракетный двигатель
RU2486113C1 (ru) * 2011-11-09 2013-06-27 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Система запуска криогенного жидкостного ракетного двигателя космического объекта
RU2476708C1 (ru) * 2011-11-25 2013-02-27 Николай Борисович Болотин Жидкостный ракетный двигатель
RU2476709C1 (ru) * 2011-11-25 2013-02-27 Николай Борисович Болотин Жидкостный ракетный двигатель
US20130199155A1 (en) * 2012-01-02 2013-08-08 Jordin Kare Rocket Propulsion Systems, and Related Methods
RU2497730C1 (ru) * 2012-04-09 2013-11-10 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Двигательная установка космического летательного аппарата (варианты) и способ ее эксплуатации
FR2998926B1 (fr) * 2012-11-30 2014-12-26 Snecma Ensemble propulsif pour fusee
CN102975869A (zh) * 2012-12-13 2013-03-20 上海宇航系统工程研究所 一种探测器推进舱及其工作方法
US20140182265A1 (en) * 2013-01-03 2014-07-03 Jordin Kare Rocket Propulsion Systems, and Related Methods
FR3000995B1 (fr) * 2013-01-11 2015-07-24 Snecma Circuit d'alimentation en ergol et procede de refroidissement
FR3000996B1 (fr) * 2013-01-11 2016-06-17 Snecma Systeme et procede d'alimentation d'un moteur-fusee
FR3009586B1 (fr) * 2013-08-06 2015-08-28 Snecma Dispositif d'alimentation en ergol de moteur-fusee
FR3009587B1 (fr) * 2013-08-06 2015-08-28 Snecma Dispositif de pressurisation de reservoirs d'ergol d'un moteur de fusee
FR3013773B1 (fr) * 2013-11-22 2019-04-05 Arianegroup Sas Dispositif d'alimentation en ergol de chambre propulsive de moteur-fusee
RU2554126C1 (ru) * 2013-12-18 2015-06-27 Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" Объединенная двигательная установка ракетного блока
FR3020044B1 (fr) * 2014-04-17 2017-11-03 Centre Nat D'etudes Spatiales (Cnes) Reservoir amovible pour charge utile spatiale et vehicule de transfert orbital, et procede de transfert orbital
FR3027349B1 (fr) * 2014-10-21 2019-08-09 Arianegroup Sas Procede d'allumage ameliore pour moteur a ergols liquides
FR3042821B1 (fr) * 2015-10-26 2017-12-01 Snecma Procede de regulation de la pression au sein d'un premier reservoir d'ergol de moteur fusee
US20180283321A1 (en) * 2017-03-24 2018-10-04 Independence-X Aerospace Sdn Bhd System for feeding liquid propellants to combustion chamber of an engine
US11346306B1 (en) * 2019-01-03 2022-05-31 Ball Aerospace & Technologies Corp. Chemical and cold gas propellant systems and methods
US11498705B1 (en) 2019-05-09 2022-11-15 Ball Aerospace & Technology Corp. On orbit fluid propellant dispensing systems and methods
CN110425415B (zh) * 2019-08-06 2021-03-19 北京空间技术研制试验中心 航天器推进增压气体在轨补加系统及补加方法
CN110535434A (zh) * 2019-08-16 2019-12-03 四川师范大学 一种供电供热一体化的太阳能光伏系统
WO2022051513A1 (en) * 2020-09-03 2022-03-10 Momentus Inc. Shared thermal capacitor in a multi-thruster system
WO2022051511A1 (en) * 2020-09-03 2022-03-10 Momentus Inc. Thermal capacitor block with integrated fluidic channels
DE102020128007A1 (de) * 2020-10-23 2022-04-28 Arianegroup Gmbh Raketenantrieb, Verfahren sowie Raumfahrzeug
RU2760369C1 (ru) * 2021-06-15 2021-11-24 Акционерное общество "Конструкторское бюро химического машиностроения имени А.М. Исаева" Жидкостная ракетная двигательная установка космического аппарата
US11945606B1 (en) 2021-10-19 2024-04-02 Ball Aerospace & Technologies Corp. Electric propulsion based spacecraft propulsion systems and methods utilizing multiple propellants
CN114607527B (zh) * 2022-03-23 2023-09-05 北京航天雷特机电工程有限公司 一种航天发动机推进剂的温控输送系统

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3136121A (en) * 1960-02-12 1964-06-09 Aerojet General Co System for pressurizing and expelling cryogenic liquids
US3597923A (en) * 1969-10-02 1971-08-10 Michael Simon Rocket propulsion system
GB2025532B (en) * 1978-07-13 1983-06-15 Sperry Rand Ltd Fuelsystems for gas generators
US4585191A (en) * 1983-12-14 1986-04-29 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Propulsion apparatus and method using boil-off gas from a cryogenic liquid
WO1987004992A1 (en) * 1986-02-18 1987-08-27 Hughes Aircraft Company Low pressure reaction control propulsion system for a spacecraft
US4880185A (en) * 1986-02-18 1989-11-14 Hughes Aircraft Company Low pressure reaction control propulsion system for a spacecraft
US4781018A (en) * 1986-06-26 1988-11-01 Rockwell International Corporation Solar thermal propulsion unit
US5251852A (en) * 1991-09-06 1993-10-12 General Electric Company Thermal fuel transfer and tank isolation to reduce unusable fuel
US5207399A (en) * 1992-03-20 1993-05-04 General Dynamics Corporation, Space Systems Division Vapor pressurization system for outer space
FR2697587B1 (fr) * 1992-11-04 1995-01-20 Europ Propulsion Système optimisé d'alimentation de moteur fusée réallumable.
US5471833A (en) * 1993-10-06 1995-12-05 Olin Corporation Rocket propellant pressurization system using high vapor pressure liquids
US6516615B1 (en) * 2001-11-05 2003-02-11 Ford Global Technologies, Inc. Hydrogen engine apparatus with energy recovery

Also Published As

Publication number Publication date
EP1241341A1 (de) 2002-09-18
EP1241341B1 (de) 2006-05-31
US6581882B2 (en) 2003-06-24
RU2282744C2 (ru) 2006-08-27
FR2822193B1 (fr) 2003-06-27
US20020139902A1 (en) 2002-10-03
DE60211774T2 (de) 2007-05-24
FR2822193A1 (fr) 2002-09-20

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