JP4179157B2 - ２段推力型ロケットモータ - Google Patents

２段推力型ロケットモータ Download PDF

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Publication number
JP4179157B2
JP4179157B2 JP2003417041A JP2003417041A JP4179157B2 JP 4179157 B2 JP4179157 B2 JP 4179157B2 JP 2003417041 A JP2003417041 A JP 2003417041A JP 2003417041 A JP2003417041 A JP 2003417041A JP 4179157 B2 JP4179157 B2 JP 4179157B2
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Japan
Prior art keywords
propellant
ignition
diaphragm
combustion chamber
igniter
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Expired - Fee Related
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JP2003417041A
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English (en)
Japanese (ja)
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JP2005171970A (ja
JP2005171970A5 (enExample
Inventor
千秋 茅野
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NOF Corp
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NOF Corp
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Priority to JP2003417041A priority Critical patent/JP4179157B2/ja
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Publication of JP2005171970A5 publication Critical patent/JP2005171970A5/ja
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JP2003417041A 2003-12-15 2003-12-15 ２段推力型ロケットモータ Expired - Fee Related JP4179157B2 (ja)

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JP2003417041A JP4179157B2 (ja) 2003-12-15 2003-12-15 ２段推力型ロケットモータ

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JP2003417041A JP4179157B2 (ja) 2003-12-15 2003-12-15 ２段推力型ロケットモータ

Publications (3)

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JP2005171970A JP2005171970A (ja) 2005-06-30
JP2005171970A5 JP2005171970A5 (enExample) 2005-10-27
JP4179157B2 true JP4179157B2 (ja) 2008-11-12

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9371801B2 (en) 2012-06-12 2016-06-21 Asahi Kasei Kabushiki Kaisha Ignition device for two-pulse rocket motor with thermal barrier membrane
KR20170141495A (ko) * 2016-06-15 2017-12-26 주식회사 한화 디스크형 점화기 마운트 조립체 및 그 설치 방법
KR101878552B1 (ko) * 2016-06-15 2018-07-13 주식회사 한화 노즐 마개형 점화기 마운트 및 그 설치 방법
KR102449276B1 (ko) 2022-04-27 2022-09-28 국방과학연구소 고고도 연소시험용 2단 펄스 추진기관

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2313685C1 (ru) * 2006-04-13 2007-12-27 Открытое акционерное общество Научно-производственное объединение "Искра" Ракетный двигатель твердого топлива
KR100823575B1 (ko) 2007-04-05 2008-04-21 국방과학연구소 고체 로켓의 추진부 구조
JP4719182B2 (ja) 2007-05-14 2011-07-06 三菱重工業株式会社 ２パルスロケットモータ
JP5602094B2 (ja) 2011-06-08 2014-10-08 三菱重工業株式会社 マルチパルスロケットモータ及びそのパルスユニット
JP5860705B2 (ja) * 2011-06-24 2016-02-16 株式会社Ｉｈｉエアロスペース パルスロケットモータ
JP5602106B2 (ja) 2011-07-14 2014-10-08 三菱重工業株式会社 燃焼ガス供給制御機構
KR101192203B1 (ko) 2012-05-08 2012-10-17 국방과학연구소 추진기관 및 이를 구비하는 로켓
JP6291343B2 (ja) * 2014-05-14 2018-03-14 株式会社Ｉｈｉエアロスペース マルチパルスロケットモータ
JP6307345B2 (ja) * 2014-05-14 2018-04-04 株式会社Ｉｈｉエアロスペース マルチパルスロケットモータとその製造方法
KR101494393B1 (ko) * 2014-05-23 2015-02-17 엘아이지넥스원 주식회사 이중 추력 로켓 추진기관
CN107529585B (zh) * 2017-03-30 2023-05-05 内蒙动力机械研究所 一种适用于多脉冲固体火箭发动机的熔膜式隔板
KR101809873B1 (ko) * 2017-05-17 2017-12-15 국방과학연구소 다중 점화 시스템
CN111305973B (zh) * 2020-03-13 2024-07-26 宁波天擎航天科技有限公司 一种小型固体火箭发动机点火装置
CN114439648B (zh) * 2021-12-31 2024-04-30 西安近代化学研究所 一种适用于发动机二次起动的火药起动器
CN114439649A (zh) * 2021-12-31 2022-05-06 西安近代化学研究所 一种有效减小占据空间的火药起动器
CN116122988B (zh) * 2022-12-12 2025-08-26 上海空间推进研究所 用于液体姿轨控动力系统的金属破裂膜片结构及使用方法
CN115853674A (zh) * 2022-12-13 2023-03-28 西安现代控制技术研究所 双脉冲发动机用环形点火器

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9371801B2 (en) 2012-06-12 2016-06-21 Asahi Kasei Kabushiki Kaisha Ignition device for two-pulse rocket motor with thermal barrier membrane
KR20170141495A (ko) * 2016-06-15 2017-12-26 주식회사 한화 디스크형 점화기 마운트 조립체 및 그 설치 방법
KR101872587B1 (ko) * 2016-06-15 2018-06-28 주식회사 한화 디스크형 점화기 마운트 조립체 및 그 설치 방법
KR101878552B1 (ko) * 2016-06-15 2018-07-13 주식회사 한화 노즐 마개형 점화기 마운트 및 그 설치 방법
KR102449276B1 (ko) 2022-04-27 2022-09-28 국방과학연구소 고고도 연소시험용 2단 펄스 추진기관

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Publication number Publication date
JP2005171970A (ja) 2005-06-30

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