DE69610285T2 - Treibstoff-Fördersystem für einen Arcjet niedriger Leistung - Google Patents

Treibstoff-Fördersystem für einen Arcjet niedriger Leistung

Info

Publication number
DE69610285T2
DE69610285T2 DE69610285T DE69610285T DE69610285T2 DE 69610285 T2 DE69610285 T2 DE 69610285T2 DE 69610285 T DE69610285 T DE 69610285T DE 69610285 T DE69610285 T DE 69610285T DE 69610285 T2 DE69610285 T2 DE 69610285T2
Authority
DE
Germany
Prior art keywords
arcjet
delivery system
low power
fuel delivery
fuel
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
DE69610285T
Other languages
English (en)
Other versions
DE69610285D1 (de
Inventor
Bernard Jackson
Robert Lewis Sackheim
Richard Aaron Rosenthal
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Northrop Grumman Space and Mission Systems Corp
Original Assignee
TRW Inc
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 TRW Inc filed Critical TRW Inc
Publication of DE69610285D1 publication Critical patent/DE69610285D1/de
Application granted granted Critical
Publication of DE69610285T2 publication Critical patent/DE69610285T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • B64G1/402—Propellant tanks; Feeding propellants
    • 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
    • B64G1/415—Arcjets or resistojets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/56—Control
    • 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
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Plasma Technology (AREA)
  • Testing Of Engines (AREA)
  • Nozzles (AREA)
  • Coating By Spraying Or Casting (AREA)
DE69610285T 1996-02-23 1996-12-20 Treibstoff-Fördersystem für einen Arcjet niedriger Leistung Expired - Fee Related DE69610285T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/606,184 US5819526A (en) 1996-02-23 1996-02-23 Low power arcjet propellant feed system

Publications (2)

Publication Number Publication Date
DE69610285D1 DE69610285D1 (de) 2000-10-19
DE69610285T2 true DE69610285T2 (de) 2001-01-18

Family

ID=24426921

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69610285T Expired - Fee Related DE69610285T2 (de) 1996-02-23 1996-12-20 Treibstoff-Fördersystem für einen Arcjet niedriger Leistung

Country Status (6)

Country Link
US (1) US5819526A (de)
EP (1) EP0791742B1 (de)
JP (1) JP3068022B2 (de)
CN (1) CN1184890A (de)
DE (1) DE69610285T2 (de)
RU (1) RU2166666C2 (de)

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WO2005003557A1 (en) * 2003-06-25 2005-01-13 Design Net Engineering, Llc Laser propulsion thruster
IL159248A (en) * 2003-12-08 2011-10-31 Aharon Oren Impulse motor with increased electro-thermal impulse
US8127527B2 (en) * 2004-11-22 2012-03-06 General Electric Company Methods and systems for operating oxidizer systems
US7690187B2 (en) * 2006-09-26 2010-04-06 The Aerospace Corporation Modular micropropulsion device and system
JP2009262770A (ja) * 2008-04-25 2009-11-12 Ihi Aerospace Co Ltd 宇宙機用推進装置
CN101907039B (zh) * 2010-07-23 2013-04-03 北京航空航天大学 一种采用三圆柱推进剂贮箱的氮气冷气微推进装置
FR2963811B1 (fr) * 2010-08-12 2012-08-31 Snecma Propulseur electrique, procede d'arret d'un moteur electrique compris dans un tel propulseur et satellite comprenant un tel propulseur
RU2466292C1 (ru) * 2011-08-23 2012-11-10 Николай Борисович Болотин Жидкостный ракетный двигатель
CN102493938B (zh) * 2011-12-30 2013-07-17 南开大学 飞船电动推进器
FR2994587B1 (fr) * 2012-08-20 2017-07-07 Snecma Allumeur bimodal et procede d'injection bimodale pour allumeur de moteur-fusee
FR2997462B1 (fr) 2012-10-30 2018-09-14 Safran Aircraft Engines Alimentation d'un propulseur ionique en gaz propulsif
US8967046B2 (en) 2012-11-30 2015-03-03 Alliant Techsystems Inc. Gas generators, launch tubes including gas generators and related systems and methods
US9546892B2 (en) * 2013-10-10 2017-01-17 The Boeing Company Methods and systems for estimation of propellant transfer in an ion propulsion system
RU2577920C1 (ru) * 2014-12-18 2016-03-20 Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" Устройство для обеспечения командного давления жидкостного ракетного двигателя с насосной подачей компонентов топлива
US10336475B1 (en) 2015-11-10 2019-07-02 Space Systems/Loral, Llc Flexible propulsion system
US10281248B2 (en) 2015-11-11 2019-05-07 Northrop Grumman Innovation Systems, Inc. Gas generators, launch tube assemblies including gas generators, and related systems and methods
CN105736270B (zh) * 2016-01-29 2018-06-08 兰州空间技术物理研究所 一种用于推进器的微小流量供气纯度控制系统
US10018072B2 (en) * 2016-05-26 2018-07-10 General Electric Company Dual trip manifold assembly for turbine systems
US10287036B2 (en) * 2016-07-08 2019-05-14 Lockheed Martin Corporation Arcjet propulsion systems for spacecraft
CN108612599B (zh) * 2016-12-10 2020-09-08 中国科学院大连化学物理研究所 一种液-电组合空间推力器
US11661907B2 (en) 2018-10-11 2023-05-30 Sierra Space Corporation Vortex hybrid rocket motor
US11572851B2 (en) * 2019-06-21 2023-02-07 Sierra Space Corporation Reaction control vortex thruster system
CN110761902A (zh) * 2019-11-05 2020-02-07 西安中科宇航动力技术有限公司 一种电动泵自增压动力系统
AU2021211979A1 (en) * 2020-08-06 2022-02-24 Dawn Aerospace Limited Rocket motor and components thereof
CN113357112A (zh) * 2021-07-02 2021-09-07 兰州空间技术物理研究所 一种推进剂供给模块及推力器起弧方法
US11952967B2 (en) 2021-08-19 2024-04-09 Sierra Space Corporation Liquid propellant injector for vortex hybrid rocket motor
CN113944573B (zh) * 2021-09-14 2022-12-13 北京控制工程研究所 一种电弧发动机和单组元发动机通用高空模拟试验系统
US11879414B2 (en) 2022-04-12 2024-01-23 Sierra Space Corporation Hybrid rocket oxidizer flow control system including regression rate sensors

Family Cites Families (19)

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Publication number Priority date Publication date Assignee Title
DE1751389A1 (de) * 1968-05-22 1971-07-08 Gerd Zelck Treibstoffoerdereinrichtung fuer ein mit mindestens einem fluessigen Treibstoff arbeitendes Raketentriebwerk
DE2059683B1 (de) * 1970-12-04 1972-05-25 Messerschmitt Boelkow Blohm Treibstoffsystem,insbesondere fuer Raketentriebwerke
US4319926A (en) * 1980-12-22 1982-03-16 Ppg Industries, Inc. Curable silicate compositions containing condensed phosphate hardeners and pH controlling bases
US4523429A (en) * 1983-04-01 1985-06-18 Rca Corporation Cold start surge current limiting system for a hydrazine thruster augmentation heater
US4548033A (en) * 1983-06-22 1985-10-22 Cann Gordon L Spacecraft optimized arc rocket
US4577461A (en) * 1983-06-22 1986-03-25 Cann Gordon L Spacecraft optimized arc rocket
US4656828A (en) * 1984-09-28 1987-04-14 Rca Corporation Augmentation heater temperature control system
US4930310A (en) * 1985-12-18 1990-06-05 Rockcor, Inc. Monopropellant plenum propulsion system with integrated valve/nozzle for fast response thrust
US4805399A (en) * 1985-12-18 1989-02-21 Rockcor Incorporated Monopropellant plenum propulsion system with integrated valve/nozzle for fast response thrust
US4800716A (en) * 1986-07-23 1989-01-31 Olin Corporation Efficiency arcjet thruster with controlled arc startup and steady state attachment
US4766724A (en) * 1987-06-10 1988-08-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Arcjet power supply and start circuit
US4882465A (en) * 1987-10-01 1989-11-21 Olin Corporation Arcjet thruster with improved arc attachment for enhancement of efficiency
US4926632A (en) * 1988-02-01 1990-05-22 Olin Corporation Performance arcjet thruster
US4995231A (en) * 1988-02-01 1991-02-26 Olin Corporation Performance arcjet thruster
DE4005607C1 (de) * 1990-02-22 1991-07-25 Erno Raumfahrttechnik Gmbh, 2800 Bremen, De
US5282357A (en) * 1990-04-19 1994-02-01 Trw Inc. High-performance dual-mode integral propulsion system
US5026259A (en) * 1990-07-09 1991-06-25 The United States Of America As Represented By The United States Department Of Energy Miniaturized pressurization system
FR2669887B1 (fr) * 1990-11-30 1995-06-02 Aerospatiale Procede de controle d'attitude en tangage d'un satellite grace a la pression de radiation solaire et satellite adapte a sa mise en óoeuvre.
US5170623A (en) * 1991-01-28 1992-12-15 Trw Inc. Hybrid chemical/electromagnetic propulsion system

Also Published As

Publication number Publication date
DE69610285D1 (de) 2000-10-19
JP3068022B2 (ja) 2000-07-24
US5819526A (en) 1998-10-13
EP0791742B1 (de) 2000-09-13
RU2166666C2 (ru) 2001-05-10
EP0791742A1 (de) 1997-08-27
CN1184890A (zh) 1998-06-17
JPH09228894A (ja) 1997-09-02

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee