JP2002540340A5 - - Google Patents

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Publication number
JP2002540340A5
JP2002540340A5 JP2000606890A JP2000606890A JP2002540340A5 JP 2002540340 A5 JP2002540340 A5 JP 2002540340A5 JP 2000606890 A JP2000606890 A JP 2000606890A JP 2000606890 A JP2000606890 A JP 2000606890A JP 2002540340 A5 JP2002540340 A5 JP 2002540340A5
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JP
Japan
Prior art keywords
rotary
flow path
inlet
outlet
shaft
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JP2000606890A
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English (en)
Japanese (ja)
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JP2002540340A (ja
JP4386589B2 (ja
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Priority claimed from PCT/US2000/006393 external-priority patent/WO2000057048A2/en
Publication of JP2002540340A publication Critical patent/JP2002540340A/ja
Publication of JP2002540340A5 publication Critical patent/JP2002540340A5/ja
Application granted granted Critical
Publication of JP4386589B2 publication Critical patent/JP4386589B2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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JP2000606890A 1999-03-10 2000-03-10 ロケットエンジン Expired - Lifetime JP4386589B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12362199P 1999-03-10 1999-03-10
US60/123,621 1999-03-10
PCT/US2000/006393 WO2000057048A2 (en) 1999-03-10 2000-03-10 Rocket engine

Related Child Applications (2)

Application Number Title Priority Date Filing Date
JP2009044656A Division JP2009150402A (ja) 1999-03-10 2009-02-26 ロケットエンジン
JP2009044653A Division JP2009150401A (ja) 1999-03-10 2009-02-26 ロケットエンジン

Publications (3)

Publication Number Publication Date
JP2002540340A JP2002540340A (ja) 2002-11-26
JP2002540340A5 true JP2002540340A5 (enExample) 2009-04-23
JP4386589B2 JP4386589B2 (ja) 2009-12-16

Family

ID=22409771

Family Applications (3)

Application Number Title Priority Date Filing Date
JP2000606890A Expired - Lifetime JP4386589B2 (ja) 1999-03-10 2000-03-10 ロケットエンジン
JP2009044653A Pending JP2009150401A (ja) 1999-03-10 2009-02-26 ロケットエンジン
JP2009044656A Ceased JP2009150402A (ja) 1999-03-10 2009-02-26 ロケットエンジン

Family Applications After (2)

Application Number Title Priority Date Filing Date
JP2009044653A Pending JP2009150401A (ja) 1999-03-10 2009-02-26 ロケットエンジン
JP2009044656A Ceased JP2009150402A (ja) 1999-03-10 2009-02-26 ロケットエンジン

Country Status (11)

Country Link
US (3) US6220016B1 (enExample)
EP (1) EP1171705B1 (enExample)
JP (3) JP4386589B2 (enExample)
CN (2) CN1201076C (enExample)
AT (1) ATE386203T1 (enExample)
AU (1) AU6045800A (enExample)
CA (1) CA2364284C (enExample)
DE (2) DE60044733D1 (enExample)
IL (4) IL145349A0 (enExample)
RU (1) RU2243403C2 (enExample)
WO (1) WO2000057048A2 (enExample)

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CN101984240B (zh) * 2010-11-11 2013-04-24 西北工业大学 一种提高脉冲爆震火箭发动机工作频率的方法及装置
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CN103742296B (zh) * 2013-12-23 2017-03-01 中国航天科技集团公司第六研究院第十一研究所 一种气膜冷却喷管
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CN104309562A (zh) * 2014-10-25 2015-01-28 陈恒兰 车用准固液推进剂火箭防护系统
CN105630002B (zh) * 2014-10-30 2018-11-02 北京精密机电控制设备研究所 一种液体火箭发动机变推力调节机电伺服机构
CN106050475A (zh) * 2016-08-03 2016-10-26 杨斯涵 一种液固耦合式火箭发动机
CN106438104B (zh) * 2016-09-18 2018-05-22 中国科学院工程热物理研究所 一种富燃预燃涡扇发动机
CN107829844B (zh) * 2017-09-28 2019-07-16 西安航天动力试验技术研究所 一种四角切圆式的注气装置
CN108131205B (zh) * 2017-11-20 2019-06-18 北京动力机械研究所 一种涡扇发动机燃烧室启动方法
CN110541758B (zh) * 2019-08-14 2024-04-12 张繁荣 一种含氧燃料用涡轮喷气发动机
AU2021211979A1 (en) * 2020-08-06 2022-02-24 Dawn Aerospace Limited Rocket motor and components thereof
CN113266492B (zh) * 2021-04-16 2022-03-15 北京星际荣耀空间科技股份有限公司 发动机推力室、火箭发动机、液体火箭
JP7039095B1 (ja) * 2021-06-17 2022-03-22 基輝 三森 ロケットエンジン用水素噴射装置
CN113882971B (zh) * 2021-09-15 2023-02-03 浙江理工大学 一种火箭发动机涡轮泵的定子导叶结构
CN114991997B (zh) * 2022-06-01 2024-09-13 西安航天动力研究所 一种身部和推力室
CN115726905B (zh) * 2022-11-16 2024-06-11 青岛星辰航线科技有限公司 一种液氧、煤油火炬式点火器
CN119844795B (zh) * 2023-10-18 2025-11-25 中国航发商用航空发动机有限责任公司 集油环、燃油喷嘴及燃烧室
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