SG10201500751UA - A micro-nozzle thruster - Google Patents

A micro-nozzle thruster

Info

Publication number
SG10201500751UA
SG10201500751UA SG10201500751UA SG10201500751UA SG10201500751UA SG 10201500751U A SG10201500751U A SG 10201500751UA SG 10201500751U A SG10201500751U A SG 10201500751UA SG 10201500751U A SG10201500751U A SG 10201500751UA SG 10201500751U A SG10201500751U A SG 10201500751UA
Authority
SG
Singapore
Prior art keywords
micro
nozzle thruster
thruster
nozzle
Prior art date
Application number
SG10201500751UA
Inventor
Giulio Manzoni
Original Assignee
Microspace Rapid Pte Ltd
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 Microspace Rapid Pte Ltd filed Critical Microspace Rapid Pte Ltd
Priority to SG10201500751UA priority Critical patent/SG10201500751UA/en
Publication of SG10201500751UA publication Critical patent/SG10201500751UA/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00Using plasma to produce a reactive propulsive thrust
    • F03H1/0037Electrostatic ion thrusters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/405Ion or plasma engines
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/411Electric propulsion
    • B64G1/413Ion or plasma engines
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/411Electric propulsion
    • B64G1/415Arcjets or resistojets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00Using plasma to produce a reactive propulsive thrust
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00Using plasma to produce a reactive propulsive thrust
    • F03H1/0037Electrostatic ion thrusters
    • F03H1/0043Electrostatic ion thrusters characterised by the acceleration grid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00Using plasma to produce a reactive propulsive thrust
    • F03H1/0037Electrostatic ion thrusters
    • F03H1/0056Electrostatic ion thrusters with an acceleration grid and an applied magnetic field
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00Using plasma to produce a reactive propulsive thrust
    • F03H1/0081Electromagnetic plasma thrusters
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00Using plasma to produce a reactive propulsive thrust
    • F03H1/0087Electro-dynamic thrusters, e.g. pulsed plasma thrusters
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00Using plasma to produce a reactive propulsive thrust
    • F03H1/0093Electro-thermal plasma thrusters, i.e. thrusters heating the particles in a plasma
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05HPLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
    • H05H1/00Generating plasma; Handling plasma
    • H05H1/24Generating plasma
    • H05H1/48Generating plasma using an arc
    • H05H1/50Generating plasma using an arc and using applied magnetic fields, e.g. for focusing or rotating the arc
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05HPLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
    • H05H1/00Generating plasma; Handling plasma
    • H05H1/54Plasma accelerators
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B81MICROSTRUCTURAL TECHNOLOGY
    • B81BMICROSTRUCTURAL DEVICES OR SYSTEMS, e.g. MICROMECHANICAL DEVICES
    • B81B2201/00Specific applications of microelectromechanical systems
    • B81B2201/03Microengines and actuators
    • B81B2201/038Microengines and actuators not provided for in B81B2201/031 - B81B2201/037

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)
  • Electromagnetism (AREA)
  • Optics & Photonics (AREA)
  • Plasma Technology (AREA)
SG10201500751UA 2010-02-08 2011-02-08 A micro-nozzle thruster SG10201500751UA (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SG10201500751UA SG10201500751UA (en) 2010-02-08 2011-02-08 A micro-nozzle thruster

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SG2010009108 2010-02-08
SG10201500751UA SG10201500751UA (en) 2010-02-08 2011-02-08 A micro-nozzle thruster

Publications (1)

Publication Number Publication Date
SG10201500751UA true SG10201500751UA (en) 2015-04-29

Family

ID=55167961

Family Applications (2)

Application Number Title Priority Date Filing Date
SG2012058582A SG182846A1 (en) 2010-02-08 2011-02-08 A micro-nozzle thruster
SG10201500751UA SG10201500751UA (en) 2010-02-08 2011-02-08 A micro-nozzle thruster

Family Applications Before (1)

Application Number Title Priority Date Filing Date
SG2012058582A SG182846A1 (en) 2010-02-08 2011-02-08 A micro-nozzle thruster

Country Status (4)

Country Link
US (1) US9410539B2 (en)
EP (1) EP2534051A4 (en)
SG (2) SG182846A1 (en)
WO (1) WO2011096899A1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102701139A (en) * 2012-05-06 2012-10-03 西北工业大学 Preparation method of solid state chemistry micro-propeller
US9334068B2 (en) 2014-04-04 2016-05-10 NOA Inc. Unified orbit and attitude control for nanosatellites using pulsed ablative thrusters
RU2551408C1 (en) * 2014-06-24 2015-05-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Самарский государственный аэрокосмический университет имени академика С.П. Королева" (национальный исследовательский университет)" (СГАУ) Device for controlled lunching of nano- and microsatellites
CN104401507B (en) * 2014-10-21 2016-08-17 上海微小卫星工程中心 A kind of cold air micro-thruster
US10287036B2 (en) * 2016-07-08 2019-05-14 Lockheed Martin Corporation Arcjet propulsion systems for spacecraft
CN108590993B (en) * 2018-03-19 2019-08-09 上海空间推进研究所 A kind of 80mN hall thruster micrometeor distributor
CN114320670A (en) * 2021-12-22 2022-04-12 杭州热力科技有限公司 Engine spray pipe flow control device and method using plasma

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1243798B (en) * 1963-08-19 1967-07-06 Snecma Electrothermal jet nozzle
US3537266A (en) * 1968-01-22 1970-11-03 Gen Dynamics Corp Ion engine thrust multiplier
FR2421534A1 (en) * 1973-10-02 1979-10-26 Delcroix Jean Loup LARGE CROSS-SECTION PLASMA SOURCE, CONSTITUTING AN ION ACCELERATOR
US4577461A (en) * 1983-06-22 1986-03-25 Cann Gordon L Spacecraft optimized arc rocket
US4548033A (en) * 1983-06-22 1985-10-22 Cann Gordon L Spacecraft optimized arc rocket
GB2149456B (en) * 1983-11-08 1987-07-29 Rolls Royce Exhaust mixing in turbofan aeroengines
US4800716A (en) * 1986-07-23 1989-01-31 Olin Corporation Efficiency arcjet thruster with controlled arc startup and steady state attachment
US4733530A (en) * 1986-08-04 1988-03-29 Hughes Aircraft Company Emission current control system for multiple hollow cathode devices
US4882465A (en) * 1987-10-01 1989-11-21 Olin Corporation Arcjet thruster with improved arc attachment for enhancement of efficiency
US5076051A (en) * 1990-02-06 1991-12-31 Olin Corporation Long life arcjet thruster having diffuse cathode arc attachment
DE4122755A1 (en) * 1991-07-10 1993-01-21 Erno Raumfahrttechnik Gmbh ENGINE FOR SPACING BODIES
US5836150A (en) * 1995-05-31 1998-11-17 The United States Of America As Represented By The United States Department Of Energy Micro thrust and heat generator
US5826150A (en) * 1997-07-14 1998-10-20 Xerox Corporation Integrated multi-toner dispensing system
EP1173874A4 (en) 1999-03-31 2007-04-11 Science Res Lab Inc Plasma gun and methods for the use thereof
US6216445B1 (en) 1999-05-19 2001-04-17 Trw Inc. Micro pulsed plasma thruster and method of operating same
WO2003007311A1 (en) 2001-07-09 2003-01-23 W.E. Research Llc Description of methods to increase propellant throughput in a micro pulsed plasma thruster
US7227097B2 (en) * 2002-05-08 2007-06-05 Btu International, Inc. Plasma generation and processing with multiple radiation sources
US7302792B2 (en) * 2003-10-16 2007-12-04 The Johns Hopkins University Pulsed plasma thruster and method of making
DE102007006444B4 (en) * 2007-02-05 2015-05-13 Airbus Defence and Space GmbH Micro-engine, in particular for use as attitude control engine, small engine and method for manufacturing a micro-engine
US8613188B2 (en) * 2008-05-14 2013-12-24 Purdue Research Foundation Method of enhancing microthruster performance
ES1071088Y (en) * 2009-09-18 2010-04-07 Ebanisteria Aguera S A PANEL FIXING DEVICE

Also Published As

Publication number Publication date
US20120318886A1 (en) 2012-12-20
EP2534051A4 (en) 2017-04-05
WO2011096899A1 (en) 2011-08-11
EP2534051A1 (en) 2012-12-19
US9410539B2 (en) 2016-08-09
SG182846A1 (en) 2012-09-27

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