JPH11324797A5 - - Google Patents
Info
- Publication number
- JPH11324797A5 JPH11324797A5 JP1999118964A JP11896499A JPH11324797A5 JP H11324797 A5 JPH11324797 A5 JP H11324797A5 JP 1999118964 A JP1999118964 A JP 1999118964A JP 11896499 A JP11896499 A JP 11896499A JP H11324797 A5 JPH11324797 A5 JP H11324797A5
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- oxidizer
- injection element
- igniter
- insert
- 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.)
- Pending
Links
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/069133 | 1998-04-29 | ||
| US09/069,133 US6082098A (en) | 1998-04-29 | 1998-04-29 | Ignition system for rocket engines |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH11324797A JPH11324797A (ja) | 1999-11-26 |
| JPH11324797A5 true JPH11324797A5 (enExample) | 2006-06-15 |
Family
ID=22086964
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP11118964A Pending JPH11324797A (ja) | 1998-04-29 | 1999-04-27 | ロケットエンジン用点火システム |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6082098A (enExample) |
| EP (1) | EP0953759B1 (enExample) |
| JP (1) | JPH11324797A (enExample) |
| KR (1) | KR100532170B1 (enExample) |
| DE (1) | DE69914824T2 (enExample) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6082098A (en) * | 1998-04-29 | 2000-07-04 | United Technologies Corporation | Ignition system for rocket engines |
| EP1172545B1 (de) | 2000-07-15 | 2013-05-29 | Astrium GmbH | Zündsystem für Brennkammern in Raketentriebwerken |
| US6860099B1 (en) * | 2003-01-09 | 2005-03-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Liquid propellant tracing impingement injector |
| US6918243B2 (en) * | 2003-05-19 | 2005-07-19 | The Boeing Company | Bi-propellant injector with flame-holding zone igniter |
| US7565795B1 (en) * | 2006-01-17 | 2009-07-28 | Pratt & Whitney Rocketdyne, Inc. | Piezo-resonance igniter and ignition method for propellant liquid rocket engine |
| US8122703B2 (en) | 2006-04-28 | 2012-02-28 | United Technologies Corporation | Coaxial ignition assembly |
| US20080264372A1 (en) * | 2007-03-19 | 2008-10-30 | Sisk David B | Two-stage ignition system |
| US20080299504A1 (en) * | 2007-06-01 | 2008-12-04 | Mark David Horn | Resonance driven glow plug torch igniter and ignition method |
| US20090235636A1 (en) * | 2008-03-21 | 2009-09-24 | Robert Oehrlein | Reinforced, regeneratively cooled uni-body rocket engine |
| US8814562B2 (en) * | 2008-06-02 | 2014-08-26 | Aerojet Rocketdyne Of De, Inc. | Igniter/thruster with catalytic decomposition chamber |
| US8161725B2 (en) * | 2008-09-22 | 2012-04-24 | Pratt & Whitney Rocketdyne, Inc. | Compact cyclone combustion torch igniter |
| CN102400815B (zh) * | 2011-03-18 | 2013-09-18 | 北京航空航天大学 | 一种气氧和甲烷小推力发动机层板式喷注器 |
| FR3037619B1 (fr) * | 2015-06-22 | 2017-06-30 | Snecma | Allumeur de moteur - fusee retractable |
| RU175861U1 (ru) * | 2017-03-21 | 2017-12-21 | Публичное акционерное общество "Научно-производственное объединение "Сатурн" | Камера сгорания жидкостного ракетного двигателя |
| CN110242439B (zh) * | 2019-05-06 | 2021-02-09 | 上海空间推进研究所 | 基于层板扩散焊的发动机喷注器、制造方法以及发动机 |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3085393A (en) * | 1958-06-03 | 1963-04-16 | North American Aviation Inc | Rocket engine starting method |
| US3106059A (en) * | 1961-03-30 | 1963-10-08 | United Aircraft Corp | Oxidizer inlet and igniter for a rocket |
| US3468487A (en) * | 1966-02-28 | 1969-09-23 | Us Navy | Variable thrust injector |
| US3662960A (en) * | 1966-11-21 | 1972-05-16 | United Aircraft Corp | Injector head |
| US4707982A (en) * | 1981-06-26 | 1987-11-24 | Rockwell International Corporation | Thermal regenerative injector |
| US4621492A (en) * | 1985-01-10 | 1986-11-11 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Low loss injector for liquid propellant rocket engines |
| JPH0192560A (ja) * | 1987-10-02 | 1989-04-11 | Natl Aerospace Lab | ロケット噴射器 |
| US5172548A (en) * | 1988-09-14 | 1992-12-22 | Societe Europeene De Propulsion | Device for tapping off hot gases from a combustion chamber and injector head equipped with such a device |
| US5109669A (en) * | 1989-09-28 | 1992-05-05 | Rockwell International Corporation | Passive self-contained auto ignition system |
| DE4305154C1 (de) * | 1993-02-19 | 1994-05-26 | Deutsche Aerospace | Einspritzelement in Koaxialbauweise für Raketenbrennkammern |
| US6082098A (en) * | 1998-04-29 | 2000-07-04 | United Technologies Corporation | Ignition system for rocket engines |
-
1998
- 1998-04-29 US US09/069,133 patent/US6082098A/en not_active Expired - Fee Related
-
1999
- 1999-04-26 KR KR10-1999-0014838A patent/KR100532170B1/ko not_active Expired - Fee Related
- 1999-04-27 JP JP11118964A patent/JPH11324797A/ja active Pending
- 1999-04-29 EP EP99303351A patent/EP0953759B1/en not_active Expired - Lifetime
- 1999-04-29 DE DE69914824T patent/DE69914824T2/de not_active Expired - Fee Related
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