BRPI0409043A - propulsor de nave espacial e processo para a geração de impulsão - Google Patents
propulsor de nave espacial e processo para a geração de impulsãoInfo
- Publication number
- BRPI0409043A BRPI0409043A BRPI0409043-8A BRPI0409043A BRPI0409043A BR PI0409043 A BRPI0409043 A BR PI0409043A BR PI0409043 A BRPI0409043 A BR PI0409043A BR PI0409043 A BRPI0409043 A BR PI0409043A
- Authority
- BR
- Brazil
- Prior art keywords
- magnetic field
- generates
- chamber
- tube
- resonant cavity
- 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
- F03H1/0081—Electromagnetic plasma thrusters
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- Electromagnetism (AREA)
- Plasma & Fusion (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Plasma Technology (AREA)
- Particle Accelerators (AREA)
- Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
- Liquid Crystal Substances (AREA)
- Two-Way Televisions, Distribution Of Moving Picture Or The Like (AREA)
Abstract
"PROPULSOR DE NAVE ESPACIAL E PROCESSO PARA A GERAçãO DE IMPULSãO". Um propulsor tem uma câmara (6) definida dentro de um tubo (2). O tubo tem um eixo geométrico longitudinal que define um eixo (4) de impulsão; um injetor (8) injeta um gás ionizável dentro do tubo, em uma extremidade da câmara. Um gerador de campo magnético com duas bobinas (12, 14) gera um campo magnético paralelo ao eixo geométrico; o campo magnético tem dois valores máximos ao longo do eixo geométrico (4); um gerador de campo eletromagnético tem uma primeira cavidade ressonante (16) entre as duas bobinas que gera um campo de ionização de microondas à ressonância do ciclotron de elétrons na câmara (6), entre os dois valores máximos do campo magnético. O gerador de campo eletromagnético tem uma segunda cavidade ressonante (18) no outro lado da segunda bobina (14). A segunda cavidade ressonante (18) gera um campo de aceleração ponderomotiva que acelera o gás ionizado. O propulsor ioniza o gás pela ressonância do ciclotron de elétrons, e acelera subseqüentemente os elétrons e os íons pela força ponderomotiva magnetizada.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP03290712A EP1460267B1 (en) | 2003-03-20 | 2003-03-20 | Spacecraft thruster |
| PCT/US2004/008054 WO2005028310A2 (en) | 2003-03-20 | 2004-03-17 | Spacecraft thruster |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BRPI0409043A true BRPI0409043A (pt) | 2006-03-28 |
Family
ID=32799136
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0409043-8A BRPI0409043A (pt) | 2003-03-20 | 2004-03-17 | propulsor de nave espacial e processo para a geração de impulsão |
Country Status (14)
| Country | Link |
|---|---|
| EP (2) | EP1460267B1 (pt) |
| JP (1) | JP4977459B2 (pt) |
| KR (1) | KR101075218B1 (pt) |
| CN (1) | CN1761816B (pt) |
| AT (1) | ATE335928T1 (pt) |
| AU (1) | AU2004274389B2 (pt) |
| BR (1) | BRPI0409043A (pt) |
| CA (1) | CA2519701C (pt) |
| DE (1) | DE60307418T2 (pt) |
| ES (1) | ES2272909T3 (pt) |
| IL (1) | IL170820A (pt) |
| MX (1) | MXPA05009982A (pt) |
| RU (1) | RU2330181C2 (pt) |
| WO (1) | WO2005028310A2 (pt) |
Families Citing this family (40)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2295797B1 (en) * | 2004-09-22 | 2013-01-23 | Elwing LLC | Spacecraft thruster |
| US7509795B2 (en) * | 2005-01-13 | 2009-03-31 | Lockheed-Martin Corporation | Systems and methods for plasma propulsion |
| KR100698618B1 (ko) | 2005-07-12 | 2007-03-22 | 삼성전자주식회사 | 플라즈마 가속장치 및 그것을 구비하는 플라즈마 처리시스템 |
| AU2007219050B2 (en) * | 2006-02-24 | 2013-05-30 | Jozef Goj | System to propel fluid matter in an elongate flow tube |
| DE102006059264A1 (de) * | 2006-12-15 | 2008-06-19 | Thales Electron Devices Gmbh | Plasmabeschleunigeranordnung |
| RU2403440C1 (ru) * | 2009-02-13 | 2010-11-10 | Открытое акционерное общество "АВИАЦИОННАЯ ЭЛЕКТРОНИКА И КОММУНИКАЦИОННЫЕ СИСТЕМЫ ОАО "АВЭКС" | Способ управления расходом ионизационной плазмы при регулировании тяги электрореактивного двигателя малой тяги |
| CN102782320B (zh) * | 2010-03-01 | 2015-01-28 | 三菱电机株式会社 | 霍尔推进器及宇宙航行体及推进方法 |
| RU2011129508A (ru) * | 2011-07-18 | 2012-02-20 | Закрытое акционерное общество "Техмаш" (RU) | Способ создания пондеромоторного эффекта воздействия и "аннигиляционные" движители |
| FR2985292B1 (fr) * | 2011-12-29 | 2014-01-24 | Onera (Off Nat Aerospatiale) | Propulseur plasmique et procede de generation d'une poussee propulsive plasmique |
| CN102767496B (zh) * | 2012-05-22 | 2014-12-03 | 北京卫星环境工程研究所 | 化学-电磁混合可变比冲的推进器 |
| CN102767497B (zh) * | 2012-05-22 | 2014-06-18 | 北京卫星环境工程研究所 | 基于空间原子氧的无燃料航天器推进系统及推进方法 |
| RU2518467C2 (ru) * | 2012-06-05 | 2014-06-10 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Ионная двигательная установка космических аппаратов |
| CN102797656B (zh) * | 2012-08-03 | 2014-08-13 | 北京卫星环境工程研究所 | 吸气式螺旋波电推进装置 |
| CN103037609B (zh) * | 2013-01-10 | 2014-12-31 | 哈尔滨工业大学 | 射流等离子体电子能量调节器 |
| CN103052249A (zh) * | 2013-01-11 | 2013-04-17 | 哈尔滨工业大学 | 一种射流等离子体密度分布调节器 |
| JP2013137024A (ja) * | 2013-01-30 | 2013-07-11 | Elwing Llc | スラスタ及びそのシステム、そして推進発生方法 |
| JP6345413B2 (ja) * | 2013-11-22 | 2018-06-20 | 学校法人立命館 | 深紫外発光素子 |
| JP2014194220A (ja) * | 2014-06-12 | 2014-10-09 | Elwing Llc | スラスタ及び推進発生方法 |
| CN104061137B (zh) * | 2014-07-11 | 2016-10-05 | 哈尔滨工业大学 | 根据地面实验参数修正在轨飞行霍尔推力器推力参数的方法 |
| CN104454417B (zh) * | 2014-10-29 | 2017-04-12 | 大连理工大学 | 双阶栅极螺旋波离子推进装置 |
| CN104653422B (zh) * | 2015-01-22 | 2017-04-12 | 大连理工大学 | 三级加速式螺旋波等离子体推进装置 |
| JP6661012B2 (ja) | 2015-11-18 | 2020-03-11 | ジェイエスダブリュー スチール リミテッド | 宇宙空間電熱推進に適したマイクロ波電熱スラスタ |
| CN105554995B (zh) * | 2015-12-18 | 2018-12-14 | 中国科学院西安光学精密机械研究所 | 高密度等离子体发生装置 |
| CN105781921B (zh) * | 2016-03-16 | 2018-06-19 | 中国空间技术研究院 | 一种基于周期结构的电磁推力器腔体 |
| CN105781793B (zh) * | 2016-03-29 | 2017-10-03 | 兰州理工大学 | 一种喷气引擎核心机 |
| WO2019226358A2 (en) * | 2018-05-09 | 2019-11-28 | Alpha Ring International Ltd. | Electron and ion cyclotron resonance enabled fusion reactors |
| CN111120232B (zh) * | 2018-11-01 | 2021-08-03 | 哈尔滨工业大学 | 一种可实现微调控放电性能的会切场等离子体推力器 |
| CN109681398B (zh) * | 2018-12-12 | 2020-08-28 | 上海航天控制技术研究所 | 一种新型微波ecr离子推力器放电室 |
| CN110132606B (zh) * | 2019-05-28 | 2020-06-19 | 北京航空航天大学 | 推力器羽流参数测量系统、方法及装置 |
| CN110337170B (zh) * | 2019-07-11 | 2021-06-22 | 哈尔滨工业大学 | 一种基于电流驱动技术反场位形结构的高密度等离子体射流发生装置 |
| CN111140454B (zh) * | 2020-02-13 | 2021-05-04 | 哈尔滨工业大学 | 一种微型电子回旋共振离子推力器点火装置 |
| CN111392070A (zh) * | 2020-04-24 | 2020-07-10 | 北京卫星环境工程研究所 | 一种基于射频电离的气体收集装置 |
| CN111706480A (zh) * | 2020-06-18 | 2020-09-25 | 哈尔滨工业大学 | 一种基于电场加速的离子风推力装置 |
| GB2609465A (en) * | 2021-08-03 | 2023-02-08 | Magdrive Ltd | Thrust vectoring system |
| CN114352494B (zh) * | 2021-12-15 | 2024-12-27 | 西安航天动力研究所 | 基于多级磁场及多段喷管的等离子体生成装置及方法 |
| CN116301025B (zh) * | 2023-02-01 | 2025-07-15 | 中国西安卫星测控中心 | 利用多次引力辅助进行大范围倾角改变的轨道设计方法 |
| WO2025042296A1 (en) * | 2023-08-23 | 2025-02-27 | Victoria Link Limited | Magnetic field generator for a thrust assembly |
| IT202400003463A1 (it) * | 2024-02-19 | 2025-08-19 | Celeste S R L | Propulsore elettrico per uso spaziale |
| CN118011357B (zh) * | 2024-04-08 | 2024-06-14 | 中国科学院地质与地球物理研究所 | 基于非相干散射雷达提取低纬电离层e区风场的方法 |
| CN118705932B (zh) * | 2024-05-31 | 2026-01-27 | 中北大学 | 一种不同形状线圈交替组合使推进体旋转推进的方法 |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3279175A (en) * | 1962-12-19 | 1966-10-18 | Rca Corp | Apparatus for generating and accelerating charged particles |
| FR2147497A5 (pt) * | 1971-07-29 | 1973-03-09 | Commissariat Energie Atomique | |
| US3956885A (en) | 1974-09-03 | 1976-05-18 | Avco Corporation | Electrothermal reactor |
| US4328667A (en) | 1979-03-30 | 1982-05-11 | The European Space Research Organisation | Field-emission ion source and ion thruster apparatus comprising such sources |
| US4305247A (en) | 1979-06-18 | 1981-12-15 | Hughes Aircraft Company | Electrothermally augmented hydrazine thruster |
| US4663932A (en) * | 1982-07-26 | 1987-05-12 | Cox James E | Dipolar force field propulsion system |
| US4893470A (en) * | 1985-09-27 | 1990-01-16 | The United States Of America As Represented By The Administrator, National Aeronautics And Space Administration | Method of hybrid plume plasma propulsion |
| US4893089A (en) * | 1988-09-14 | 1990-01-09 | Harris Blake Corporation | Pulse power linac |
| IT1246684B (it) * | 1991-03-07 | 1994-11-24 | Proel Tecnologie Spa | Propulsore ionico a risonanza ciclotronica. |
| JPH08284803A (ja) | 1995-04-10 | 1996-10-29 | Toshiba Corp | イオンエンジン |
| IL126413A0 (en) * | 1996-04-01 | 1999-05-09 | Int Scient Products | A hall effect plasma accelerator |
| US5947421A (en) * | 1997-07-09 | 1999-09-07 | Beattie; John R. | Electrostatic propulsion systems and methods |
| US5841237A (en) * | 1997-07-14 | 1998-11-24 | Lockheed Martin Energy Research Corporation | Production of large resonant plasma volumes in microwave electron cyclotron resonance ion sources |
| DE19828704A1 (de) * | 1998-06-26 | 1999-12-30 | Thomson Tubes Electroniques Gm | Plasmabeschleuniger-Anordnung |
| US6293090B1 (en) * | 1998-07-22 | 2001-09-25 | New England Space Works, Inc. | More efficient RF plasma electric thruster |
| US6193194B1 (en) * | 1998-09-01 | 2001-02-27 | Michael A. Minovitch | Magnetic propulsion system and operating method |
| DE10153723A1 (de) * | 2001-10-31 | 2003-05-15 | Thales Electron Devices Gmbh | Plasmabeschleuniger-Anordnung |
-
2003
- 2003-03-20 AT AT03290712T patent/ATE335928T1/de not_active IP Right Cessation
- 2003-03-20 DE DE60307418T patent/DE60307418T2/de not_active Expired - Lifetime
- 2003-03-20 EP EP03290712A patent/EP1460267B1/en not_active Expired - Lifetime
- 2003-03-20 ES ES03290712T patent/ES2272909T3/es not_active Expired - Lifetime
-
2004
- 2004-03-17 EP EP04809320A patent/EP1604111A4/en not_active Withdrawn
- 2004-03-17 MX MXPA05009982A patent/MXPA05009982A/es active IP Right Grant
- 2004-03-17 WO PCT/US2004/008054 patent/WO2005028310A2/en not_active Ceased
- 2004-03-17 AU AU2004274389A patent/AU2004274389B2/en not_active Ceased
- 2004-03-17 JP JP2006509247A patent/JP4977459B2/ja not_active Expired - Fee Related
- 2004-03-17 BR BRPI0409043-8A patent/BRPI0409043A/pt not_active IP Right Cessation
- 2004-03-17 RU RU2005132306/06A patent/RU2330181C2/ru not_active IP Right Cessation
- 2004-03-17 CN CN2004800074495A patent/CN1761816B/zh not_active Expired - Fee Related
- 2004-03-17 CA CA002519701A patent/CA2519701C/en not_active Expired - Fee Related
-
2005
- 2005-09-12 IL IL170820A patent/IL170820A/en not_active IP Right Cessation
- 2005-09-15 KR KR1020057017301A patent/KR101075218B1/ko not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CA2519701A1 (en) | 2005-03-31 |
| JP4977459B2 (ja) | 2012-07-18 |
| RU2330181C2 (ru) | 2008-07-27 |
| IL170820A (en) | 2010-04-29 |
| CN1761816B (zh) | 2010-06-23 |
| DE60307418T2 (de) | 2007-03-29 |
| ATE335928T1 (de) | 2006-09-15 |
| CA2519701C (en) | 2008-12-30 |
| KR101075218B1 (ko) | 2011-10-19 |
| DE60307418D1 (de) | 2006-09-21 |
| EP1460267A1 (en) | 2004-09-22 |
| KR20050120762A (ko) | 2005-12-23 |
| AU2004274389B2 (en) | 2011-03-17 |
| JP2007524784A (ja) | 2007-08-30 |
| EP1460267B1 (en) | 2006-08-09 |
| AU2004274389A1 (en) | 2005-03-31 |
| RU2005132306A (ru) | 2006-02-10 |
| EP1604111A4 (en) | 2006-01-18 |
| EP1604111A2 (en) | 2005-12-14 |
| ES2272909T3 (es) | 2007-05-01 |
| WO2005028310A3 (en) | 2005-08-11 |
| CN1761816A (zh) | 2006-04-19 |
| MXPA05009982A (es) | 2006-03-09 |
| WO2005028310A2 (en) | 2005-03-31 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 12A ANUIDADE. |
|
| B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2370 DE 07-06-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |