IN2013CN01336A - - Google Patents
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- Publication number
- IN2013CN01336A IN2013CN01336A IN1336CHN2013A IN2013CN01336A IN 2013CN01336 A IN2013CN01336 A IN 2013CN01336A IN 1336CHN2013 A IN1336CHN2013 A IN 1336CHN2013A IN 2013CN01336 A IN2013CN01336 A IN 2013CN01336A
- Authority
- IN
- India
- Prior art keywords
- motor
- low pressure
- buffer tank
- tank
- pressure buffer
- Prior art date
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
- B64G1/411—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)
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 |
|---|---|
| IN2013CN01336A true IN2013CN01336A (enExample) | 2015-08-07 |
Family
ID=43948123
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IN1336CHN2013 IN2013CN01336A (enExample) | 2010-08-12 | 2011-07-27 |
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)
| 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)
| 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 |
-
2010
- 2010-08-12 FR FR1056577A patent/FR2963811B1/fr active Active
-
2011
- 2011-07-27 IN IN1336CHN2013 patent/IN2013CN01336A/en unknown
- 2011-07-27 RU RU2013105150/06A patent/RU2562338C2/ru active
- 2011-07-27 US US13/816,408 patent/US9003767B2/en active Active
- 2011-07-27 JP JP2013523652A patent/JP5809699B2/ja active Active
- 2011-07-27 EP EP11752308.4A patent/EP2603698B1/fr active Active
- 2011-07-27 UA UAA201301630A patent/UA108113C2/ru unknown
- 2011-07-27 WO PCT/FR2011/051812 patent/WO2012020190A1/fr not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| RU2013105150A (ru) | 2014-09-20 |
| FR2963811B1 (fr) | 2012-08-31 |
| 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 |
| JP5809699B2 (ja) | 2015-11-11 |
| WO2012020190A1 (fr) | 2012-02-16 |
| EP2603698A1 (fr) | 2013-06-19 |
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