UA108113C2 - Електроракетна рушійна установка, спосіб зупинки електроракетного двигуна в такій установці і супутник, що містить таку установку - Google Patents

Електроракетна рушійна установка, спосіб зупинки електроракетного двигуна в такій установці і супутник, що містить таку установку

Info

Publication number
UA108113C2
UA108113C2 UAA201301630A UAA201301630A UA108113C2 UA 108113 C2 UA108113 C2 UA 108113C2 UA A201301630 A UAA201301630 A UA A201301630A UA A201301630 A UAA201301630 A UA A201301630A UA 108113 C2 UA108113 C2 UA 108113C2
Authority
UA
Ukraine
Prior art keywords
installation
electric rocket
low pressure
stoping
buffer tank
Prior art date
Application number
UAA201301630A
Other languages
English (en)
Ukrainian (uk)
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 filed Critical
Publication of UA108113C2 publication Critical patent/UA108113C2/ru

Links

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
    • B64G1/405—Ion or plasma 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
    • B64G1/411—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)
UAA201301630A 2010-08-12 2011-07-27 Електроракетна рушійна установка, спосіб зупинки електроракетного двигуна в такій установці і супутник, що містить таку установку UA108113C2 (uk)

Applications Claiming Priority (2)

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
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 (1)

Publication Number Publication Date
UA108113C2 true UA108113C2 (uk) 2015-03-25

Family

ID=43948123

Family Applications (1)

Application Number Title Priority Date Filing Date
UAA201301630A UA108113C2 (uk) 2010-08-12 2011-07-27 Електроракетна рушійна установка, спосіб зупинки електроракетного двигуна в такій установці і супутник, що містить таку установку

Country Status (8)

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

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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
EP3620394A1 (en) * 2018-09-06 2020-03-11 Airbus Defence and Space Limited A propulsion system
US20210309396A1 (en) * 2018-09-06 2021-10-07 Airbus Defence And Space Limited A propulsion system
CN112768332A (zh) * 2019-11-05 2021-05-07 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

Family Cites Families (11)

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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 (ru) * 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
US6286304B1 (en) 1998-09-23 2001-09-11 Mainstream Engineering Corporation Noble gas storage and delivery system for ion propulsion
US6301876B1 (en) * 1998-09-23 2001-10-16 Mainstream Engineering Corporation Noble gas storage and flow control 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
JP2013536356A (ja) 2013-09-19
RU2562338C2 (ru) 2015-09-10
IN2013CN01336A (ru) 2015-08-07
JP5809699B2 (ja) 2015-11-11
EP2603698A1 (fr) 2013-06-19
EP2603698B1 (fr) 2015-10-07
RU2013105150A (ru) 2014-09-20
FR2963811B1 (fr) 2012-08-31
US9003767B2 (en) 2015-04-14
FR2963811A1 (fr) 2012-02-17
US20130200219A1 (en) 2013-08-08
WO2012020190A1 (fr) 2012-02-16

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