KR20160055169A - 전기적으로 점화되고 스로틀링되는 초전성 추진제 로켓 엔진 - Google Patents

전기적으로 점화되고 스로틀링되는 초전성 추진제 로켓 엔진 Download PDF

Info

Publication number
KR20160055169A
KR20160055169A KR1020167008182A KR20167008182A KR20160055169A KR 20160055169 A KR20160055169 A KR 20160055169A KR 1020167008182 A KR1020167008182 A KR 1020167008182A KR 20167008182 A KR20167008182 A KR 20167008182A KR 20160055169 A KR20160055169 A KR 20160055169A
Authority
KR
South Korea
Prior art keywords
propellant
electrode
electrically
electrically ignitable
combustion
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.)
Withdrawn
Application number
KR1020167008182A
Other languages
English (en)
Korean (ko)
Inventor
마이클 디. 맥퍼슨
Original Assignee
디지털 솔리드 스테이트 프로펄젼 인크.
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 디지털 솔리드 스테이트 프로펄젼 인크. filed Critical 디지털 솔리드 스테이트 프로펄젼 인크.
Publication of KR20160055169A publication Critical patent/KR20160055169A/ko
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • 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
    • F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements
    • 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
    • F02K9/52—Injectors
    • 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
    • F02K9/94—Re-ignitable or restartable rocket- engine plants; Intermittently operated rocket-engine plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
KR1020167008182A 2013-08-29 2014-08-29 전기적으로 점화되고 스로틀링되는 초전성 추진제 로켓 엔진 Withdrawn KR20160055169A (ko)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201361871767P 2013-08-29 2013-08-29
US61/871,767 2013-08-29
PCT/US2014/053528 WO2015031825A1 (en) 2013-08-29 2014-08-29 Electrically ignited and throttled pyroelectric propellant rocket engine

Publications (1)

Publication Number Publication Date
KR20160055169A true KR20160055169A (ko) 2016-05-17

Family

ID=52581231

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020167008182A Withdrawn KR20160055169A (ko) 2013-08-29 2014-08-29 전기적으로 점화되고 스로틀링되는 초전성 추진제 로켓 엔진

Country Status (5)

Country Link
US (1) US20150059314A1 (enExample)
EP (1) EP3039277A4 (enExample)
JP (1) JP2016536520A (enExample)
KR (1) KR20160055169A (enExample)
WO (1) WO2015031825A1 (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10532830B2 (en) * 2016-06-09 2020-01-14 The Boeing Company Stackable pancake satellite
CN107044362B (zh) * 2016-12-07 2018-12-11 西安近代化学研究所 一种低羽焰特征发动机
CN111502860B (zh) * 2020-04-30 2022-06-28 南京理工大学 一种模块化设计的压力旋流喷注器
DE102020122337A1 (de) * 2020-08-26 2022-03-03 LabOrbital GmbH Heißgaserzeugungsvorrichtung mit monergolem ionischen Treibstoff und Niederspannungsanzündung
CN112796907B (zh) * 2021-01-05 2021-12-14 南京理工大学 一种镁凝胶二氧化碳发动机
CN114592989B (zh) * 2022-05-09 2022-08-16 西安航天动力研究所 一种液氧煤油针栓喷注器推力室及其启动方法
CN115263604B (zh) * 2022-06-22 2024-10-01 北京控制工程研究所 一种应用于轻质快响双组元发动机的对孔互击喷注器
CN115324772B (zh) * 2022-07-28 2024-05-31 北京控制工程研究所 一种双组元推力器推进剂混合比预测方法

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3057149A (en) * 1958-09-30 1962-10-09 Aerojet General Co Rocket propellant spark ignition system
US3790088A (en) * 1967-08-29 1974-02-05 Us Army Propellant splash plate having flow directing means
US3651644A (en) * 1969-06-25 1972-03-28 Marshall Ind Apparatus for initiating decomposition of an exothermic propellant
FR2497273B1 (fr) * 1980-12-29 1985-09-20 Onera (Off Nat Aerospatiale) Procede et dispositif pour allumage d'un melange carbure
US5395076A (en) * 1993-03-19 1995-03-07 Martin Marietta Corporation Spacecraft velocity change maneuvers by variable arcjets
US6469424B1 (en) * 1998-12-14 2002-10-22 United Technologies Corporation Ignitor for liquid fuel rocket engines
AU2003304725A1 (en) * 2002-01-16 2008-05-29 W.E. Research, Llc Electrically controlled extinguishable solid propellant motors
US6931832B2 (en) * 2003-05-13 2005-08-23 United Technologies Corporation Monopropellant combustion system
US7246483B2 (en) * 2004-07-21 2007-07-24 United Technologies Corporation Energetic detonation propulsion
US8337765B2 (en) * 2005-08-26 2012-12-25 Honeywell International Inc. Electrocatalytically induced propellant decomposition
US7634903B2 (en) * 2005-10-12 2009-12-22 Richard Cary Phillips Ion impulse engine
US8122703B2 (en) * 2006-04-28 2012-02-28 United Technologies Corporation Coaxial ignition assembly
US8230672B2 (en) * 2006-12-04 2012-07-31 Firestar Engineering, Llc Spark-integrated propellant injector head with flashback barrier
FR2914369B1 (fr) * 2007-03-30 2014-02-07 Snecma Allumeur electrolytique pour moteur-fusee a monergol
US8857338B2 (en) * 2008-05-16 2014-10-14 Digital Solid State Propulsion Llc Electrode ignition and control of electrically ignitable materials

Also Published As

Publication number Publication date
EP3039277A4 (en) 2017-04-26
WO2015031825A1 (en) 2015-03-05
US20150059314A1 (en) 2015-03-05
EP3039277A1 (en) 2016-07-06
JP2016536520A (ja) 2016-11-24

Similar Documents

Publication Publication Date Title
KR20160055169A (ko) 전기적으로 점화되고 스로틀링되는 초전성 추진제 로켓 엔진
US7770380B2 (en) Methods of controlling solid propellant ignition, combustion, and extinguishment
US8776526B2 (en) Motor with solid fuel installed within combustion chamber and vortex generator installed on inner wall of combustion chamber
US7788900B2 (en) Electrically controlled extinguishable solid propellant motors
CN109595100B (zh) 一种电点火绿色单元液体火箭发动机结构
US20130139487A1 (en) Variable initiation location system for pulse detonation combustor
JP7603675B2 (ja) 宇宙船用ハイブリッド推進装置
US11480136B1 (en) Monopropellant continuous detonation engines
US7194852B1 (en) Propulsion from combustion of solid propellant pellet-projectiles
US11408376B2 (en) Thrust augmentation of an additively manufactured hybrid rocket system using secondary oxidizer injection
CN108688829A (zh) 固液动力亚轨道运载火箭
US6968676B1 (en) Propulsion from combustion of solid propellant pellet-projectiles
JP2007192221A (ja) ロケットエンジン用のアコースティックキャビティマニフォルド、ロケットエンジン及びロケットエンジンの比推力効率を向上させる方法
Tsay et al. Development of Busek 0.5 N green monopropellant thruster
US20130139486A1 (en) Variable initiation location system for pulse detonation combustor
US20220348360A1 (en) Miniaturized green end-burning hybrid propulsion system for cubesats
Jung et al. Autoignitable and restartable hybrid rockets using catalytic decomposition of an oxidizer
US7506500B1 (en) Propulsion from combustion of solid propellant pellet-projectiles
US20240125287A1 (en) Monopropellant continuous detonation engines
Liu et al. A long duration and high reliability liquid apogee engine for satellites
Heister et al. Survey of rotating detonation wave combustor technology and potential rocket vehicle applications
Venugopal et al. Hybrid rocket technology
EP3951157B1 (en) Rocket motor and components thereof
Pinto et al. Green gelled propellant highly throtteable rocket motor and gas generator technology: status and application
Bzdyk et al. Investigation of the operating parameters and performance of an autophage, hybrid rocket propulsion system

Legal Events

Date Code Title Description
PA0105 International application

Patent event date: 20160328

Patent event code: PA01051R01D

Comment text: International Patent Application

PG1501 Laying open of application
PC1203 Withdrawal of no request for examination
WITN Application deemed withdrawn, e.g. because no request for examination was filed or no examination fee was paid