PL3724497T3 - Jonowy silnik rakietowy - Google Patents

Jonowy silnik rakietowy

Info

Publication number
PL3724497T3
PL3724497T3 PL18753043T PL18753043T PL3724497T3 PL 3724497 T3 PL3724497 T3 PL 3724497T3 PL 18753043 T PL18753043 T PL 18753043T PL 18753043 T PL18753043 T PL 18753043T PL 3724497 T3 PL3724497 T3 PL 3724497T3
Authority
PL
Poland
Prior art keywords
ion thruster
thruster
ion
Prior art date
Application number
PL18753043T
Other languages
English (en)
Inventor
Nembo Buldrini
Florin PLESESCU
Original Assignee
Enpulsion Gmbh
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 Enpulsion Gmbh filed Critical Enpulsion Gmbh
Publication of PL3724497T3 publication Critical patent/PL3724497T3/pl

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
    • 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
    • F03H1/005—Electrostatic ion thrusters using field emission, e.g. Field Emission Electric Propulsion [FEEP]
PL18753043T 2017-12-12 2018-07-24 Jonowy silnik rakietowy PL3724497T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
AT601382017 2017-12-12
PCT/AT2018/060159 WO2019113617A1 (en) 2017-12-12 2018-07-24 Ion thruster
EP18753043.1A EP3724497B1 (en) 2017-12-12 2018-07-24 Ion thruster

Publications (1)

Publication Number Publication Date
PL3724497T3 true PL3724497T3 (pl) 2022-04-04

Family

ID=63168216

Family Applications (1)

Application Number Title Priority Date Filing Date
PL18753043T PL3724497T3 (pl) 2017-12-12 2018-07-24 Jonowy silnik rakietowy

Country Status (11)

Country Link
US (1) US11365726B2 (pl)
EP (1) EP3724497B1 (pl)
CN (1) CN111566345B (pl)
AU (1) AU2018384065A1 (pl)
DK (1) DK3724497T3 (pl)
HU (1) HUE057314T2 (pl)
LT (1) LT3724497T (pl)
PL (1) PL3724497T3 (pl)
PT (1) PT3724497T (pl)
RU (1) RU2764497C2 (pl)
WO (1) WO2019113617A1 (pl)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11359613B1 (en) * 2020-06-02 2022-06-14 United States Of America As Represented By The Secretary Of The Air Force Electrospray thruster with inverted geometry
EP4276307A1 (en) * 2022-05-12 2023-11-15 ENPULSION GmbH Liquid metal ion source
EP4276306A1 (en) * 2022-05-12 2023-11-15 ENPULSION GmbH Ion source
CN115355145A (zh) * 2022-07-25 2022-11-18 北京控制工程研究所 一种基于气体场电离增强的微牛级变推力器

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4328667A (en) 1979-03-30 1982-05-11 The European Space Research Organisation Field-emission ion source and ion thruster apparatus comprising such sources
JPS6011417B2 (ja) * 1979-10-23 1985-03-26 株式会社東芝 ホロ−カソ−ド放電装置
WO1999063222A1 (en) * 1998-06-05 1999-12-09 Primex Aerospace Company Uniform gas distribution in ion accelerators with closed electron drift
US6516604B2 (en) * 2000-03-27 2003-02-11 California Institute Of Technology Micro-colloid thruster system
AT500412B8 (de) 2002-12-23 2007-02-15 Arc Seibersdorf Res Gmbh Flüssigmetall-ionenquelle
US6996972B2 (en) 2004-05-18 2006-02-14 The Boeing Company Method of ionizing a liquid propellant and an electric thruster implementing such a method
US8030621B2 (en) 2007-06-08 2011-10-04 Massachusetts Institute Of Technology Focused ion beam field source
US7827779B1 (en) * 2007-09-10 2010-11-09 Alameda Applied Sciences Corp. Liquid metal ion thruster array
US8791411B2 (en) * 2008-05-06 2014-07-29 Massachusetts Institute Of Technology Method and apparatus for a porous electrospray emitter
WO2011079138A2 (en) 2009-12-21 2011-06-30 California Institute Of Technology Microfluidic electrospray thruster
US8207496B2 (en) 2010-02-05 2012-06-26 Thermo Finnigan Llc Multi-needle multi-parallel nanospray ionization source for mass spectrometry
US10308377B2 (en) 2011-05-03 2019-06-04 Massachusetts Institute Of Technology Propellant tank and loading for electrospray thruster
CN105402099B (zh) * 2015-12-07 2018-08-03 上海空间推进研究所 一种针式多孔材料发射体阵列微型场发射电推力器
RU2672060C1 (ru) * 2018-02-09 2018-11-09 Российская Федерация, от имени которой выступает Государственная корпорация по космической деятельности "РОСКОСМОС" Катод плазменного ускорителя

Also Published As

Publication number Publication date
HUE057314T2 (hu) 2022-04-28
EP3724497A1 (en) 2020-10-21
LT3724497T (lt) 2022-01-10
AU2018384065A1 (en) 2020-06-25
RU2020122949A (ru) 2022-01-13
RU2020122949A3 (pl) 2022-01-13
CN111566345B (zh) 2023-04-07
RU2764497C2 (ru) 2022-01-17
CN111566345A (zh) 2020-08-21
US20200340459A1 (en) 2020-10-29
PT3724497T (pt) 2021-12-31
EP3724497B1 (en) 2021-11-24
WO2019113617A1 (en) 2019-06-20
DK3724497T3 (da) 2022-01-24
US11365726B2 (en) 2022-06-21

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