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DE69610285D1 - Treibstoff-Fördersystem für einen Arcjet niedriger Leistung - Google Patents

Treibstoff-Fördersystem für einen Arcjet niedriger Leistung

Info

Publication number
DE69610285D1
DE69610285D1 DE69610285T DE69610285T DE69610285D1 DE 69610285 D1 DE69610285 D1 DE 69610285D1 DE 69610285 T DE69610285 T DE 69610285T DE 69610285 T DE69610285 T DE 69610285T DE 69610285 D1 DE69610285 D1 DE 69610285D1
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
DE69610285T2 (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)
  • Nozzles (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Testing Of Engines (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 true DE69610285D1 (de) 2000-10-19
DE69610285T2 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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CN113944573A (zh) * 2021-09-14 2022-01-18 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

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US8127527B2 (en) * 2004-11-22 2012-03-06 General Electric Company Methods and systems for operating oxidizer systems
RU2331915C2 (ru) * 2005-11-22 2008-08-20 Государственное Образовательное Учреждение Высшего Профессионального Образования "Дагестанский Государственный Технический Университет" (Дгту) Генератор псевдослучайных последовательностей импульсов на однородной среде с программно меняющейся структурой
RU2319033C1 (ru) * 2006-08-01 2008-03-10 Федеральное государственное унитарное предприятие "Конструкторское бюро общего машиностроения им. В.П. Бармина" (ФГУП "КБОМ им. В.П. Бармина") Способ продувки азотом двигателей ракет-носителей и система продувки азотом двигателей ракет-носителей
US7690187B2 (en) * 2006-09-26 2010-04-06 The Aerospace Corporation Modular micropropulsion device and system
RU2326262C1 (ru) * 2006-12-21 2008-06-10 Дмитрий Александрович Новосельцев Комбинированный электрохимический ракетный двигатель
RU2328616C1 (ru) * 2006-12-25 2008-07-10 Дмитрий Александрович Новосельцев Комбинированный электрохимический ракетный двигатель
JP2009262770A (ja) * 2008-04-25 2009-11-12 Ihi Aerospace Co Ltd 宇宙機用推進装置
RU2392589C2 (ru) * 2008-06-02 2010-06-20 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ определения расхода системы подачи рабочего тела к источнику плазмы
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
US11879414B2 (en) 2022-04-12 2024-01-23 Sierra Space Corporation Hybrid rocket oxidizer flow control system including regression rate sensors
US12196158B2 (en) * 2022-10-31 2025-01-14 Phase Four, Inc. Multimode propulsion system
CN115743623B (zh) * 2022-12-16 2024-12-10 上海航天控制技术研究所 一种氧化亚氮气液复合推进系统
US20250237183A1 (en) * 2024-01-24 2025-07-24 Aerojet Rocketdyne, Inc. Warm gas thruster system with control valve that has a soft seal

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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
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113944573A (zh) * 2021-09-14 2022-01-18 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
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

Also Published As

Publication number Publication date
JPH09228894A (ja) 1997-09-02
EP0791742B1 (de) 2000-09-13
RU2166666C2 (ru) 2001-05-10
EP0791742A1 (de) 1997-08-27
CN1184890A (zh) 1998-06-17
US5819526A (en) 1998-10-13
DE69610285T2 (de) 2001-01-18
JP3068022B2 (ja) 2000-07-24

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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