ATE524646T1 - Hybridraketensystem - Google Patents
HybridraketensystemInfo
- Publication number
- ATE524646T1 ATE524646T1 AT06817596T AT06817596T ATE524646T1 AT E524646 T1 ATE524646 T1 AT E524646T1 AT 06817596 T AT06817596 T AT 06817596T AT 06817596 T AT06817596 T AT 06817596T AT E524646 T1 ATE524646 T1 AT E524646T1
- Authority
- AT
- Austria
- Prior art keywords
- hybrid rocket
- reactant
- rocket system
- rocket motor
- thrust
- Prior art date
Links
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
- F02K9/72—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants
-
- 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
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
- F02K9/26—Burning control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/05—Purpose of the control system to affect the output of the engine
- F05D2270/051—Thrust
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Testing Of Engines (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2005906887A AU2005906887A0 (en) | 2005-12-08 | Hybrid rocket system | |
PCT/AU2006/001861 WO2007065220A1 (en) | 2005-12-08 | 2006-12-07 | Hybrid rocket system |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE524646T1 true ATE524646T1 (de) | 2011-09-15 |
Family
ID=38122414
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT06817596T ATE524646T1 (de) | 2005-12-08 | 2006-12-07 | Hybridraketensystem |
Country Status (5)
Country | Link |
---|---|
US (1) | US8387361B2 (de) |
EP (1) | EP1960654B1 (de) |
AT (1) | ATE524646T1 (de) |
CA (1) | CA2633097C (de) |
WO (1) | WO2007065220A1 (de) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USRE49778E1 (en) | 2007-03-22 | 2024-01-02 | Firehawk Aerospace, Inc. | Persistent vortex generating high regression rate solid fuel grain for a hybrid rocket engine |
USRE49765E1 (en) | 2007-03-22 | 2023-12-26 | Firehawk Aerospace, Inc. | Additive manufactured thermoplastic-nanocomposite aluminum hybrid rocket fuel grain and method of manufacturing same |
KR101153989B1 (ko) | 2009-11-16 | 2012-06-08 | 한국항공대학교산학협력단 | 경사진 그레인 포트를 가진 하이브리드 로켓의 고체 연료 |
FR2995364A1 (fr) * | 2012-09-13 | 2014-03-14 | Astrium Sas | Dispositif de propulsion hybride anaerobie a carburant presente sous de forme de solides divises |
US11001384B2 (en) * | 2017-10-02 | 2021-05-11 | Bell Helicopter Textron Inc. | Hybrid power systems for aircraft |
US20210148307A1 (en) * | 2019-01-30 | 2021-05-20 | Laboratoire Reaction Dynamics Inc. | Rocket engine with integrated oxidizer catalyst in manifold and injector assembly |
WO2020154809A1 (en) | 2019-01-30 | 2020-08-06 | Laboratoire Reaction Dynamics Inc. | Rocket engines |
CN110594038B (zh) * | 2019-08-20 | 2021-11-09 | 西安航天动力技术研究所 | 一种多次脉冲激励装置 |
CN111734551B (zh) * | 2020-06-15 | 2022-08-02 | 哈尔滨工程大学 | 一种分离式多级推力的水下动力系统及其控制方法 |
CN112177797B (zh) * | 2020-09-16 | 2021-11-05 | 西北工业大学 | 一种无喷管固体火箭发动机 |
CN113202633B (zh) * | 2021-04-28 | 2022-06-07 | 中国航发沈阳发动机研究所 | 一种小涵道比一体化加力燃烧室供油规律设计方法 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2981060A (en) * | 1959-03-25 | 1961-04-25 | United Aircraft Corp | Rocket construction |
US3183665A (en) * | 1959-04-07 | 1965-05-18 | Hexcel Products Inc | Rocket grain and method of constructing same |
US3083527A (en) * | 1960-10-10 | 1963-04-02 | Phillips Petroleum Co | Hybrid rocket propulsion process |
US3166898A (en) * | 1962-01-16 | 1965-01-26 | United Aircraft Corp | Liquid injection system |
US3286471A (en) * | 1963-09-30 | 1966-11-22 | North American Aviation Inc | Solid propellant rocket motor |
FR1406001A (fr) * | 1964-06-04 | 1965-07-16 | Soc Et Propulsion Par Reaction | Moteur-fusée hybride alimenté par turbo-pompe |
US3270505A (en) * | 1964-10-21 | 1966-09-06 | Norman L Crabill | Control system for rocket vehicles |
US3325998A (en) * | 1965-04-14 | 1967-06-20 | Thiokol Chemical Corp | Variable thrust rocket motor |
US3373564A (en) * | 1966-04-26 | 1968-03-19 | Hayes Internat Corp | Process and apparatus for controlling rocket engines and the like |
US3421323A (en) * | 1966-11-14 | 1969-01-14 | Donald Perry Bennett Jr | Fluid fuel and non-fluid oxidizer energy generation method |
US3575381A (en) * | 1968-08-23 | 1971-04-20 | Dresser Ind | Valve seat construction |
DE2057327A1 (de) * | 1970-11-21 | 1972-05-31 | Licentia Gmbh | Strahltriebwerk fuer einen Flugkoerper |
US3742701A (en) * | 1971-06-16 | 1973-07-03 | Us Navy | Propellant injector assembly |
JPS56159535A (en) * | 1980-05-13 | 1981-12-08 | Nissan Motor Co Ltd | Rocket motor |
US4424679A (en) * | 1981-09-10 | 1984-01-10 | The United States Of America As Represented By The Secretary Of The Air Force | Constant thrust hybrid rocket motor |
US5394690A (en) * | 1993-09-20 | 1995-03-07 | The United States Of America As Represented By The Secretary Of The Army | Constant pressure, variable thrust bipropellant engine |
US6125763A (en) * | 1998-08-14 | 2000-10-03 | Environmental Aeroscience Corp. | Integral solid booster and hybrid thrust sustaining system and projectile incorporating the same |
US6679049B2 (en) * | 2002-01-22 | 2004-01-20 | Hy Pat Corporation | Hybrid rocket motor having a precombustion chamber |
-
2006
- 2006-12-07 US US12/086,191 patent/US8387361B2/en active Active
- 2006-12-07 CA CA2633097A patent/CA2633097C/en active Active
- 2006-12-07 EP EP06817596A patent/EP1960654B1/de active Active
- 2006-12-07 AT AT06817596T patent/ATE524646T1/de not_active IP Right Cessation
- 2006-12-07 WO PCT/AU2006/001861 patent/WO2007065220A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
CA2633097A1 (en) | 2007-06-14 |
EP1960654B1 (de) | 2011-09-14 |
US20090139204A1 (en) | 2009-06-04 |
CA2633097C (en) | 2012-09-25 |
WO2007065220A1 (en) | 2007-06-14 |
US8387361B2 (en) | 2013-03-05 |
EP1960654A4 (de) | 2009-10-28 |
EP1960654A1 (de) | 2008-08-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |