JP5809699B2 - 電気スラスタ及びかかるスラスタ内の電気エンジンの停止方法並びにかかるスラスタを有する人工衛星 - Google Patents

電気スラスタ及びかかるスラスタ内の電気エンジンの停止方法並びにかかるスラスタを有する人工衛星 Download PDF

Info

Publication number
JP5809699B2
JP5809699B2 JP2013523652A JP2013523652A JP5809699B2 JP 5809699 B2 JP5809699 B2 JP 5809699B2 JP 2013523652 A JP2013523652 A JP 2013523652A JP 2013523652 A JP2013523652 A JP 2013523652A JP 5809699 B2 JP5809699 B2 JP 5809699B2
Authority
JP
Japan
Prior art keywords
pressure
buffer tank
engine
gas
tank
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.)
Active
Application number
JP2013523652A
Other languages
English (en)
Japanese (ja)
Other versions
JP2013536356A (ja
Inventor
フレデリック マルシャンディーズ
フレデリック マルシャンディーズ
ミッシェル オベル
ミッシェル オベル
ジェラール パサゴ
ジェラール パサゴ
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 JP2013536356A publication Critical patent/JP2013536356A/ja
Application granted granted Critical
Publication of JP5809699B2 publication Critical patent/JP5809699B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00—Using plasma to produce a reactive propulsive thrust
    • F03H1/0006—Details applicable to different types of plasma thrusters
    • F03H1/0012—Means for supplying the propellant
    • 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
    • B64G1/411—Electric propulsion
    • B64G1/413—Ion or plasma engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00—Using plasma to produce a reactive propulsive thrust
    • F03H1/0006—Details applicable to different types of plasma thrusters
    • F03H1/0018—Arrangements or adaptations of power supply systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00—Using plasma to produce a reactive propulsive thrust
    • F03H1/0037—Electrostatic ion thrusters

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Plasma Technology (AREA)
  • Measuring Fluid Pressure (AREA)
JP2013523652A 2010-08-12 2011-07-27 電気スラスタ及びかかるスラスタ内の電気エンジンの停止方法並びにかかるスラスタを有する人工衛星 Active JP5809699B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1056577A FR2963811B1 (fr) 2010-08-12 2010-08-12 Propulseur electrique, procede d'arret d'un moteur electrique compris dans un tel propulseur et satellite comprenant un tel propulseur
FR1056577 2010-08-12
PCT/FR2011/051812 WO2012020190A1 (fr) 2010-08-12 2011-07-27 Propulseur electrique, procede d'arret d'un moteur electrique compris dans un tel propulseur et satellite comprenant un tel propulseur

Publications (2)

Publication Number Publication Date
JP2013536356A JP2013536356A (ja) 2013-09-19
JP5809699B2 true JP5809699B2 (ja) 2015-11-11

Family

ID=43948123

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013523652A Active JP5809699B2 (ja) 2010-08-12 2011-07-27 電気スラスタ及びかかるスラスタ内の電気エンジンの停止方法並びにかかるスラスタを有する人工衛星

Country Status (8)

Country Link
US (1) US9003767B2 (enExample)
EP (1) EP2603698B1 (enExample)
JP (1) JP5809699B2 (enExample)
FR (1) FR2963811B1 (enExample)
IN (1) IN2013CN01336A (enExample)
RU (1) RU2562338C2 (enExample)
UA (1) UA108113C2 (enExample)
WO (1) WO2012020190A1 (enExample)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2997462B1 (fr) 2012-10-30 2018-09-14 Safran Aircraft Engines Alimentation d'un propulseur ionique en gaz propulsif
US9086060B1 (en) * 2012-10-31 2015-07-21 The Boeing Company Telemetry for testing switch configuration in ion propulsion system
US9181934B2 (en) * 2012-11-21 2015-11-10 The Boeing Company Rotary switch assembly for ion propulsion system
JP6214874B2 (ja) * 2013-01-22 2017-10-18 国立大学法人 東京大学 イオンエンジンのプラズマ着火用ガス供給方法及びシステム
JP6402020B2 (ja) * 2014-12-15 2018-10-10 株式会社Ｉｈｉエアロスペース 推進装置
RU2624688C2 (ru) * 2015-12-15 2017-07-05 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Устройство для измерения массы рабочего тела, газообразного при нормальных условиях, в баллоне электроракетной двигательной установки и способ определения его массы
FR3059050B1 (fr) * 2016-11-23 2019-11-29 L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Dispositif et procede de regulation de debit de gaz
EP3560298A4 (en) 2016-12-21 2020-08-12 Phase Four, Inc. PLASMA CONTROL AND PRODUCTION DEVICE
US10889389B2 (en) * 2017-04-26 2021-01-12 Marotta Controls, Inc. Electronic pressure regulation system with proportional control valve
FR3066557B1 (fr) * 2017-05-16 2019-05-10 Safran Aircraft Engines Dispositif de regulation de debit de fluide propulsif pour propulseur electrique
US11346330B1 (en) * 2017-08-24 2022-05-31 Board Of Trustees Of The University Of Alabama, For And On Behalf Of The University Of Alabama In Huntsville Additively manufactured components for electric propulsion thrusters
US20190107103A1 (en) * 2017-10-09 2019-04-11 Phase Four, Inc. Electrothermal radio frequency thruster and components
US20210309396A1 (en) * 2018-09-06 2021-10-07 Airbus Defence And Space Limited A propulsion system
EP3620394A1 (en) * 2018-09-06 2020-03-11 Airbus Defence and Space Limited A propulsion system
WO2021046044A1 (en) 2019-09-04 2021-03-11 Phase Four, Inc. Propellant injector system for plasma production devices and thrusters
CN112768332B (zh) * 2019-11-05 2024-07-05 中微半导体设备(上海)股份有限公司 一种气体输送系统及半导体处理装置
US12601331B1 (en) 2023-03-09 2026-04-14 Board Of Trustees Of The University Of Alabama, For And On Behalf Of The University Of Alabama In Huntsville Additively manufactured components for electric propulsion thrusters

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3988566A (en) * 1972-06-05 1976-10-26 Metco Inc. Automatic plasma flame spraying process and apparatus
JPS6297275U (enExample) * 1985-12-09 1987-06-20
WO1990014668A2 (en) * 1989-05-04 1990-11-29 Cravens Dennis J Cold fusion propulsion apparatus and energy generating apparatus
GB9127433D0 (en) * 1991-12-27 1992-02-19 Matra Marconi Space Uk Propulsion system for spacecraft
US5819526A (en) * 1996-02-23 1998-10-13 Trw Inc. Low power arcjet propellant feed system
US6301876B1 (en) * 1998-09-23 2001-10-16 Mainstream Engineering Corporation Noble gas storage and flow control system for ion propulsion
US6286304B1 (en) 1998-09-23 2001-09-11 Mainstream Engineering Corporation Noble gas storage and delivery system for ion propulsion
DE19948229C1 (de) * 1999-10-07 2001-05-03 Daimler Chrysler Ag Hochfrequenz-Ionenquelle
RU2339846C2 (ru) * 2006-10-23 2008-11-27 Открытое акционерное общество "Научно-производственный центр "Полюс" (ОАО "НПЦ Полюс") Способ регулирования тока анода электрореактивного плазменного двигателя и устройство для его осуществления
DE102007044071A1 (de) 2007-09-14 2009-04-02 Thales Electron Devices Gmbh Antriebsanordnung in einem Raumflugkörper
RU2371605C1 (ru) * 2008-06-16 2009-10-27 Федеральное государственное унитарное предприятие "Опытное конструкторское бюро "Факел" Плазменный двигатель с замкнутым дрейфом электронов

Also Published As

Publication number Publication date
RU2013105150A (ru) 2014-09-20
FR2963811B1 (fr) 2012-08-31
IN2013CN01336A (enExample) 2015-08-07
US20130200219A1 (en) 2013-08-08
US9003767B2 (en) 2015-04-14
UA108113C2 (uk) 2015-03-25
EP2603698B1 (fr) 2015-10-07
FR2963811A1 (fr) 2012-02-17
JP2013536356A (ja) 2013-09-19
RU2562338C2 (ru) 2015-09-10
WO2012020190A1 (fr) 2012-02-16
EP2603698A1 (fr) 2013-06-19

Similar Documents

Publication Publication Date Title
JP2013536356A (ja) 電気スラスタ及びかかるスラスタ内の電気エンジンの停止方法並びにかかるスラスタを有する人工衛星
US11530690B2 (en) Ignition process for narrow channel hall thruster
US9347438B2 (en) Hall-effect thruster
US12157586B2 (en) Propulsion system for spacecraft
KR101524641B1 (ko) 우주선의 구동 장치
JP5096893B2 (ja) マイクロ波イオン源装置
US6031334A (en) Method and apparatus for selectively distributing power in a thruster system
JP2013089307A (ja) インジェクタ付き減圧弁およびこれを備えた燃料電池システム
JP6214874B2 (ja) イオンエンジンのプラズマ着火用ガス供給方法及びシステム
US20140231669A1 (en) Microwave ion source and method for starting same
JP4263555B2 (ja) 燃料電池システムの起動方法
JP7404134B2 (ja) Ｐｉｇイオン源装置およびイオン源ガス供給システム
US12344404B2 (en) Device for regulating the rate of flow of propellant fluid for an electric thruster
CN120251474B (zh) 一种具有预电离功能的射频等离子体t形磁喷微推力器
Han et al. Unstable discharge phenomenon and stabilization of Hall thruster operating in self-excited mode
Piefer Helium Ion Source for D-3He Converged Core Operation

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20140422

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20150127

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20150216

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20150410

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20150812

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20150911

R150 Certificate of patent or registration of utility model

Ref document number: 5809699

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

S111 Request for change of ownership or part of ownership

Free format text: JAPANESE INTERMEDIATE CODE: R313113

S533 Written request for registration of change of name

Free format text: JAPANESE INTERMEDIATE CODE: R313533

R350 Written notification of registration of transfer

Free format text: JAPANESE INTERMEDIATE CODE: R350

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250