JP2016536520A - 電気的に点火され、スロットル調整された焦電性推進剤ロケットエンジン - Google Patents

電気的に点火され、スロットル調整された焦電性推進剤ロケットエンジン Download PDF

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Publication number
JP2016536520A
JP2016536520A JP2016537912A JP2016537912A JP2016536520A JP 2016536520 A JP2016536520 A JP 2016536520A JP 2016537912 A JP2016537912 A JP 2016537912A JP 2016537912 A JP2016537912 A JP 2016537912A JP 2016536520 A JP2016536520 A JP 2016536520A
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Japan
Prior art keywords
propellant
electrode
electrically
electrically ignitable
ignitable propellant
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Japanese (ja)
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JP2016536520A5 (enExample
Inventor
マイケル ディー． マクファーソン，
マイケル ディー． マクファーソン，
Original Assignee
デジタル ソリッド ステート プロパルション， インコーポレイテッド
デジタル ソリッド ステート プロパルション， インコーポレイテッド
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Application filed by デジタル ソリッド ステート プロパルション， インコーポレイテッド, デジタル ソリッド ステート プロパルション， インコーポレイテッド filed Critical デジタル ソリッド ステート プロパルション， インコーポレイテッド
Publication of JP2016536520A publication Critical patent/JP2016536520A/ja
Publication of JP2016536520A5 publication Critical patent/JP2016536520A5/ja
Pending legal-status Critical Current

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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)
JP2016537912A 2013-08-29 2014-08-29 電気的に点火され、スロットル調整された焦電性推進剤ロケットエンジン Pending JP2016536520A (ja)

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 (2)

Publication Number Publication Date
JP2016536520A true JP2016536520A (ja) 2016-11-24
JP2016536520A5 JP2016536520A5 (enExample) 2017-05-25

Family

ID=52581231

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2016537912A Pending JP2016536520A (ja) 2013-08-29 2014-08-29 電気的に点火され、スロットル調整された焦電性推進剤ロケットエンジン

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)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2023544084A (ja) * 2020-08-26 2023-10-20 ラボルビタル ゲーエムベーハー イオン性単元推進剤を用いて低圧で点火する高温ガス発生装置

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* 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
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

Citations (13)

* 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
US3651644A (en) * 1969-06-25 1972-03-28 Marshall Ind Apparatus for initiating decomposition of an exothermic propellant
US3790088A (en) * 1967-08-29 1974-02-05 Us Army Propellant splash plate having flow directing means
JPS6316644B2 (enExample) * 1980-12-29 1988-04-11 France Etat
US5395076A (en) * 1993-03-19 1995-03-07 Martin Marietta Corporation Spacecraft velocity change maneuvers by variable arcjets
JP2000179402A (ja) * 1998-12-14 2000-06-27 United Technol Corp <Utc> 液体燃料エンジン用イグナイタ
JP2004340148A (ja) * 2003-05-13 2004-12-02 United Technol Corp <Utc> 単元推進薬の燃焼のための装置および方法
JP2006046332A (ja) * 2004-07-21 2006-02-16 United Technol Corp <Utc> 推進装置および推進力発生方法
JP2007298031A (ja) * 2006-04-28 2007-11-15 United Technol Corp <Utc> 二元推進剤インジェクタ、ロケットスラスタアセンブリ、およびインジェクタアセンブリ
US20070280865A1 (en) * 2005-08-26 2007-12-06 Honeywell International, Inc. Electrically induced propellant decomposition
US20080092521A1 (en) * 2002-01-16 2008-04-24 Michael Dulligan Electrically controlled extinguishable solid propellant motors
JP2010511830A (ja) * 2006-12-04 2010-04-15 ファイアースター エンジニアリング，エルエルシー フラッシュバックバリアを備えた火花一体型推進薬噴射器ヘッド
JP4908629B2 (ja) * 2007-03-30 2012-04-04 スネクマ 単元推進薬を用いるロケットエンジン用の電解式点火器

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7634903B2 (en) * 2005-10-12 2009-12-22 Richard Cary Phillips Ion impulse engine
US8857338B2 (en) * 2008-05-16 2014-10-14 Digital Solid State Propulsion Llc Electrode ignition and control of electrically ignitable materials

Patent Citations (13)

* 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
JPS6316644B2 (enExample) * 1980-12-29 1988-04-11 France Etat
US5395076A (en) * 1993-03-19 1995-03-07 Martin Marietta Corporation Spacecraft velocity change maneuvers by variable arcjets
JP2000179402A (ja) * 1998-12-14 2000-06-27 United Technol Corp <Utc> 液体燃料エンジン用イグナイタ
US20080092521A1 (en) * 2002-01-16 2008-04-24 Michael Dulligan Electrically controlled extinguishable solid propellant motors
JP2004340148A (ja) * 2003-05-13 2004-12-02 United Technol Corp <Utc> 単元推進薬の燃焼のための装置および方法
JP2006046332A (ja) * 2004-07-21 2006-02-16 United Technol Corp <Utc> 推進装置および推進力発生方法
US20070280865A1 (en) * 2005-08-26 2007-12-06 Honeywell International, Inc. Electrically induced propellant decomposition
JP2007298031A (ja) * 2006-04-28 2007-11-15 United Technol Corp <Utc> 二元推進剤インジェクタ、ロケットスラスタアセンブリ、およびインジェクタアセンブリ
JP2010511830A (ja) * 2006-12-04 2010-04-15 ファイアースター エンジニアリング，エルエルシー フラッシュバックバリアを備えた火花一体型推進薬噴射器ヘッド
JP4908629B2 (ja) * 2007-03-30 2012-04-04 スネクマ 単元推進薬を用いるロケットエンジン用の電解式点火器

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2023544084A (ja) * 2020-08-26 2023-10-20 ラボルビタル ゲーエムベーハー イオン性単元推進剤を用いて低圧で点火する高温ガス発生装置

Also Published As

Publication number Publication date
KR20160055169A (ko) 2016-05-17
EP3039277A4 (en) 2017-04-26
WO2015031825A1 (en) 2015-03-05
US20150059314A1 (en) 2015-03-05
EP3039277A1 (en) 2016-07-06

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