RU2017130327A3 - - Google Patents
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- Publication number
- RU2017130327A3 RU2017130327A3 RU2017130327A RU2017130327A RU2017130327A3 RU 2017130327 A3 RU2017130327 A3 RU 2017130327A3 RU 2017130327 A RU2017130327 A RU 2017130327A RU 2017130327 A RU2017130327 A RU 2017130327A RU 2017130327 A3 RU2017130327 A3 RU 2017130327A3
- Authority
- RU
- Russia
Links
Classifications
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- 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
- F03H1/0062—Electrostatic ion thrusters grid-less with an applied magnetic field
-
- 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
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- 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
-
- 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
- F03H1/0062—Electrostatic ion thrusters grid-less with an applied magnetic field
- F03H1/0068—Electrostatic ion thrusters grid-less with an applied magnetic field with a central channel, e.g. end-Hall type
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05H—PLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
- H05H1/00—Generating plasma; Handling plasma
- H05H1/54—Plasma accelerators
-
- 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
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)
- Spectroscopy & Molecular Physics (AREA)
- Plasma Technology (AREA)
- Dc Machiner (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1550745A FR3032325A1 (fr) | 2015-01-30 | 2015-01-30 | Propulseur a effet hall et engin spatial comprenant un tel propulseur |
| FR1550745 | 2015-01-30 | ||
| PCT/FR2016/050186 WO2016120570A1 (fr) | 2015-01-30 | 2016-01-28 | Propulseur a effet hall et engin spatial comprenant un tel propulseur |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| RU2017130327A RU2017130327A (ru) | 2019-02-28 |
| RU2017130327A3 true RU2017130327A3 (enExample) | 2019-08-15 |
| RU2703870C2 RU2703870C2 (ru) | 2019-10-22 |
Family
ID=53404652
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2017130327A RU2703870C2 (ru) | 2015-01-30 | 2016-01-28 | Двигатель на эффекте холла и космическое транспортное средство, включающее в себя такой двигатель |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US10131453B2 (enExample) |
| EP (1) | EP3250822B1 (enExample) |
| JP (1) | JP6693967B2 (enExample) |
| CN (1) | CN107207100B (enExample) |
| FR (1) | FR3032325A1 (enExample) |
| IL (1) | IL253659B (enExample) |
| RU (1) | RU2703870C2 (enExample) |
| WO (1) | WO2016120570A1 (enExample) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3038663B1 (fr) * | 2015-07-08 | 2019-09-13 | Safran Aircraft Engines | Propulseur a effet hall exploitable en haute altitude |
| CN107939625B (zh) * | 2017-11-13 | 2019-04-05 | 中国人民解放军国防科技大学 | 反射式激光-电磁场耦合推力器 |
| CN115681062B (zh) * | 2023-01-03 | 2023-06-02 | 国科大杭州高等研究院 | 混合工作模式霍尔推进系统及具有其的航天器 |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3151259A (en) * | 1959-08-18 | 1964-09-29 | Gen Electric | Plasma accelerator system |
| RU1796777C (ru) * | 1991-06-28 | 1993-02-23 | Опытное конструкторское бюро "Факел" | Стационарный плазменный двигатель |
| RU2092983C1 (ru) * | 1996-04-01 | 1997-10-10 | Исследовательский центр им.М.В.Келдыша | Плазменный ускоритель |
| RU2088802C1 (ru) * | 1995-12-09 | 1997-08-27 | Исследовательский центр им.М.В.Келдыша | Холловский двигатель |
| CA2250913C (en) * | 1996-04-01 | 2005-06-28 | International Scientific Products | A hall effect plasma accelerator |
| US6834492B2 (en) * | 2001-06-21 | 2004-12-28 | Busek Company, Inc. | Air breathing electrically powered hall effect thruster |
| US7459858B2 (en) * | 2004-12-13 | 2008-12-02 | Busek Company, Inc. | Hall thruster with shared magnetic structure |
| US8006939B2 (en) * | 2006-11-22 | 2011-08-30 | Lockheed Martin Corporation | Over-wing traveling-wave axial flow plasma accelerator |
| FR2911956B1 (fr) * | 2007-01-29 | 2009-05-08 | Hispano Suiza Sa | Dispositif de mesure de la position d'un piston dans un cylindre, ensemble d'un cylindre, d'un piston et d'un tel dispositif et moteur d'aeronef comprenant un tel ensemble |
| JP2008223655A (ja) * | 2007-03-14 | 2008-09-25 | Japan Aerospace Exploration Agency | ホール型電気推進機 |
| FR2959534B1 (fr) * | 2010-04-29 | 2012-07-13 | Snecma | Moteur a effet hall avec regulation de la temperature du dispositif de chauffage de la cathode |
| FR2982914B1 (fr) * | 2011-11-22 | 2014-01-17 | Snecma | Propulseur a effet de hall |
| FR2986577B1 (fr) * | 2012-02-06 | 2016-05-20 | Snecma | Propulseur a effet hall |
-
2015
- 2015-01-30 FR FR1550745A patent/FR3032325A1/fr active Pending
-
2016
- 2016-01-28 US US15/547,360 patent/US10131453B2/en active Active
- 2016-01-28 JP JP2017540140A patent/JP6693967B2/ja active Active
- 2016-01-28 RU RU2017130327A patent/RU2703870C2/ru active
- 2016-01-28 CN CN201680008135.XA patent/CN107207100B/zh active Active
- 2016-01-28 WO PCT/FR2016/050186 patent/WO2016120570A1/fr not_active Ceased
- 2016-01-28 EP EP16707851.8A patent/EP3250822B1/fr active Active
-
2017
- 2017-07-25 IL IL253659A patent/IL253659B/en active IP Right Grant
Also Published As
| Publication number | Publication date |
|---|---|
| EP3250822A1 (fr) | 2017-12-06 |
| RU2703870C2 (ru) | 2019-10-22 |
| IL253659B (en) | 2021-01-31 |
| EP3250822B1 (fr) | 2019-03-13 |
| CN107207100B (zh) | 2020-05-19 |
| FR3032325A1 (fr) | 2016-08-05 |
| US20180022475A1 (en) | 2018-01-25 |
| US10131453B2 (en) | 2018-11-20 |
| JP2018503774A (ja) | 2018-02-08 |
| CN107207100A (zh) | 2017-09-26 |
| JP6693967B2 (ja) | 2020-05-13 |
| WO2016120570A1 (fr) | 2016-08-04 |
| RU2017130327A (ru) | 2019-02-28 |
| IL253659A0 (en) | 2017-09-28 |