LT3662160T - Field emission thruster and method for calibration and operation of a field emission thruster - Google Patents

Field emission thruster and method for calibration and operation of a field emission thruster

Info

Publication number
LT3662160T
LT3662160T LTEP18742465.0T LT18742465T LT3662160T LT 3662160 T LT3662160 T LT 3662160T LT 18742465 T LT18742465 T LT 18742465T LT 3662160 T LT3662160 T LT 3662160T
Authority
LT
Lithuania
Prior art keywords
field emission
emission thruster
thruster
calibration
field
Prior art date
Application number
LTEP18742465.0T
Other languages
Lithuanian (lt)
Inventor
Daniel Bock
Martin Tajmar
Philipp Laufer
Original Assignee
Morpheus Space 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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=62948114&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=LT3662160(T) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Morpheus Space Gmbh filed Critical Morpheus Space Gmbh
Publication of LT3662160T publication Critical patent/LT3662160T/en

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
    • F03H1/0037—Electrostatic ion thrusters
    • F03H1/005—Electrostatic ion thrusters using field emission, e.g. Field Emission Electric Propulsion [FEEP]

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)
  • Electron Sources, Ion Sources (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Microwave Tubes (AREA)
  • Selective Calling Equipment (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
LTEP18742465.0T 2017-07-31 2018-07-16 Field emission thruster and method for calibration and operation of a field emission thruster LT3662160T (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102017117316.1A DE102017117316B4 (en) 2017-07-31 2017-07-31 Field emission drive system and method for calibrating and operating a field emission drive system
PCT/EP2018/069251 WO2019025174A1 (en) 2017-07-31 2018-07-16 Field emission propulsion system and method for calibrating and operating a field emission propulsion system

Publications (1)

Publication Number Publication Date
LT3662160T true LT3662160T (en) 2021-09-27

Family

ID=62948114

Family Applications (1)

Application Number Title Priority Date Filing Date
LTEP18742465.0T LT3662160T (en) 2017-07-31 2018-07-16 Field emission thruster and method for calibration and operation of a field emission thruster

Country Status (8)

Country Link
EP (1) EP3662160B1 (en)
JP (1) JP7171699B2 (en)
AU (1) AU2018312508B2 (en)
CA (1) CA3071022A1 (en)
DE (1) DE102017117316B4 (en)
DK (1) DK3662160T3 (en)
LT (1) LT3662160T (en)
WO (1) WO2019025174A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3604805B1 (en) * 2018-08-02 2024-04-24 ENPULSION GmbH Ion thruster for thrust vectored propulsion of a spacecraft
DE102022103408B4 (en) 2022-02-14 2024-02-08 Technische Universität Dresden, Körperschaft des öffentlichen Rechts Electron emitters for space applications
CN115355145B (en) * 2022-07-25 2024-05-14 北京控制工程研究所 Micro-bovine-grade variable thruster based on gas field ionization enhancement

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5944754A (en) * 1982-09-06 1984-03-13 Jeol Ltd Charged particle source
US5269131A (en) 1992-08-25 1993-12-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Segmented ion thruster
US5947421A (en) * 1997-07-09 1999-09-07 Beattie; John R. Electrostatic propulsion systems and methods
JP3906549B2 (en) * 1998-02-19 2007-04-18 三菱電機株式会社 Liquid metal ion thruster
AT500412B8 (en) * 2002-12-23 2007-02-15 Arc Seibersdorf Res Gmbh LIQUID METAL ION SOURCE
JP4107391B2 (en) 2005-05-17 2008-06-25 独立行政法人 宇宙航空研究開発機構 Solid propellant thruster for space
US7690187B2 (en) 2006-09-26 2010-04-06 The Aerospace Corporation Modular micropropulsion device and system
US8453426B2 (en) * 2009-04-06 2013-06-04 Raytheon Company Current controlled field emission thruster
WO2014134386A1 (en) * 2013-03-01 2014-09-04 Michigan Technological University Generating electrospray from a ferrofluid

Also Published As

Publication number Publication date
WO2019025174A1 (en) 2019-02-07
WO2019025174A8 (en) 2019-04-18
DE102017117316A1 (en) 2019-01-31
DK3662160T3 (en) 2021-08-23
AU2018312508B2 (en) 2024-05-23
JP2020532671A (en) 2020-11-12
EP3662160A1 (en) 2020-06-10
EP3662160B1 (en) 2021-05-26
DE102017117316B4 (en) 2020-04-02
JP7171699B2 (en) 2022-11-15
AU2018312508A1 (en) 2020-01-30
CA3071022A1 (en) 2019-02-07

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