JP5711536B2 - 一酸化二窒素と燃料とが混合されて成るモノプロペラント - Google Patents
一酸化二窒素と燃料とが混合されて成るモノプロペラント Download PDFInfo
- Publication number
- JP5711536B2 JP5711536B2 JP2010533326A JP2010533326A JP5711536B2 JP 5711536 B2 JP5711536 B2 JP 5711536B2 JP 2010533326 A JP2010533326 A JP 2010533326A JP 2010533326 A JP2010533326 A JP 2010533326A JP 5711536 B2 JP5711536 B2 JP 5711536B2
- Authority
- JP
- Japan
- Prior art keywords
- monopropellant
- nofb
- dinitrogen monoxide
- fuel
- mixture
- 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.)
- Expired - Fee Related
Links
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B47/00—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase
- C06B47/02—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase the components comprising a binary propellant
- C06B47/04—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase the components comprising a binary propellant a component containing a nitrogen oxide or acid thereof
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06D—MEANS FOR GENERATING SMOKE OR MIST; GAS-ATTACK COMPOSITIONS; GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART)
- C06D5/00—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets
- C06D5/08—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets by reaction of two or more liquids
-
- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10L—FUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G, C10K; LIQUEFIED PETROLEUM GAS; ADDING MATERIALS TO FUELS OR FIRES TO REDUCE SMOKE OR UNDESIRABLE DEPOSITS OR TO FACILITATE SOOT REMOVAL; FIRELIGHTERS
- C10L3/00—Gaseous fuels; Natural gas; Synthetic natural gas obtained by processes not covered by subclass C10G, C10K; Liquefied petroleum gas
- C10L3/02—Compositions containing acetylene
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Combustion & Propulsion (AREA)
- General Chemical & Material Sciences (AREA)
- Testing Of Engines (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
Claims (19)
- ロケットエンジン用のモノプロペラントであって、一酸化二窒素と、その一酸化二窒素内に溶解する少なくとも一つのC2炭化水素系燃料との混合物を含有するモノプロペラント。
- 前記燃料は、エタン(C2H6)とエチレン(C2H4)とアセチレン(C2H2)とから成るC2グループから選択されたものである請求項1に記載のモノプロペラント。
- 酸化剤燃料比が、2.5と11.0の間にある請求項1に記載のモノプロペラント。
- 前記酸化剤燃料比は、4.0と8.0の間にある請求項3に記載のモノプロペラント。
- 前記酸化剤燃料比は、4.5と7.5との間にある請求項4に記載のモノプロペラント。
- ロケットエンジン用のモノプロペラントであって、一酸化二窒素と、その一酸化二窒素内に溶解するエタンとの混合物を、酸化剤燃料比が2.5と11.0の間にあるように含有するモノプロペラント。
- 前記酸化剤燃料比は、3.0と9.0の間にある請求項6に記載のモノプロペラント。
- 前記酸化剤燃料比は、4.0と8.0との間にある請求項7に記載のモノプロペラント。
- 前記酸化剤燃料比は、4.5と7.5との間にある請求項8に記載のモノプロペラント。
- ロケットエンジン用のモノプロペラントであって、一酸化二窒素と、その一酸化二窒素内に溶解するアセチレンとの混合物を、酸化剤燃料比が2.5と11.0との間にあるように含有するモノプロペラント。
- 前記酸化剤燃料比は、3.0と9.0との間にある請求項10に記載のモノプロペラント。
- 前記酸化剤燃料比は、4.0と8.0との間にある請求項11に記載のモノプロペラント。
- 前記酸化剤燃料比は、4.5と7.5との間にある請求項12に記載のモノプロペラント。
- 当該モノプロペラントの30%より少ない別の成分を含有する請求項1に記載のモノプロペラント。
- ロケットエンジン用のモノプロペラントを製造する方法であって、
一酸化二窒素と、少なくとも一つのC2炭化水素系燃料とを気相状態で混合し、それにより、前記一酸化二窒素と前記燃料との混合物を製造する混合工程と、
その製造された混合物を液体に凝縮させ、それにより、前記モノプロペラントを製造する凝縮工程と
を含む方法。 - ロケットエンジン用のモノプロペラントを製造する方法であって、
一酸化二窒素と、少なくとも一つのC2炭化水素系燃料とを液相状態で混合し、それにより、前記一酸化二窒素と前記燃料との混合物として前記モノプロペラントを製造する混合工程を含む方法。 - ロケットエンジン用モノプロペラントを製造する方法であって、
一酸化二窒素と、少なくとも一つのC2炭化水素系燃料とを、気相と液相とが混在する状態で混合し、それにより、前記一酸化二窒素と前記燃料との混合物として前記モノプロペラントを製造する混合工程を含む方法。 - 前記ロケットエンジンは、循環冷却式(regeneratively cooled)エンジンであり、
その循環冷却エンジンにおいては、当該モノプロペラントがクーラントとして燃焼室の壁内のジャケットを通過して流れ、それにより、前記燃焼室を冷却するとともに、当該モノプロペラントが続いて前記燃焼室に戻されて噴射され、それにより、ロケット推進のために燃焼される請求項1ないし14のいずれかに記載のモノプロペラント。 - 前記ロケットエンジンは、循環冷却式(regeneratively cooled)エンジンであり、
その循環冷却エンジンにおいては、当該モノプロペラントがクーラントとして燃焼室の壁内のジャケットを通過して流れ、それにより、前記燃焼室を冷却するとともに、当該モノプロペラントが続いて前記燃焼室に戻されて噴射され、それにより、ロケット推進のために燃焼される請求項15ないし17のいずれかに記載の方法。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US98699107P | 2007-11-09 | 2007-11-09 | |
US60/986,991 | 2007-11-09 | ||
PCT/US2008/083039 WO2009062183A1 (en) | 2007-11-09 | 2008-11-10 | Nitrous oxide fuel blend monopropellants |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2011502935A JP2011502935A (ja) | 2011-01-27 |
JP5711536B2 true JP5711536B2 (ja) | 2015-05-07 |
Family
ID=40626235
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2010533326A Expired - Fee Related JP5711536B2 (ja) | 2007-11-09 | 2008-11-10 | 一酸化二窒素と燃料とが混合されて成るモノプロペラント |
Country Status (6)
Country | Link |
---|---|
US (1) | US20090133788A1 (ja) |
EP (1) | EP2209876A4 (ja) |
JP (1) | JP5711536B2 (ja) |
CN (1) | CN101855325A (ja) |
AU (1) | AU2008323666A1 (ja) |
WO (1) | WO2009062183A1 (ja) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008123895A2 (en) | 2006-12-04 | 2008-10-16 | Firestar Engineering, Llc | Spark-integrated propellant injector head with flashback barrier |
US20120279197A1 (en) * | 2007-12-04 | 2012-11-08 | Firestar Engineering, Llc | Nitrous oxide flame barrier |
US8413419B2 (en) * | 2008-12-08 | 2013-04-09 | Firestar Engineering, Llc | Regeneratively cooled porous media jacket |
WO2011005895A1 (en) * | 2009-07-07 | 2011-01-13 | Firestar Engineering Llc | Aluminum porous media |
CN102803681A (zh) * | 2010-01-20 | 2012-11-28 | 火星工程有限公司 | 隔热燃烧室 |
AU2011218161B9 (en) * | 2010-02-16 | 2015-08-27 | David Randolph Smith | Method and apparatus to release energy in a well |
WO2011152912A2 (en) * | 2010-03-12 | 2011-12-08 | Firestar Engineering, Llc | Supersonic combustor rocket nozzle |
EP2552859A4 (en) * | 2010-04-02 | 2015-02-25 | Firestar Engineering Llc | DECOMPOSITION WITH LOW SPECIFIC EMISSION |
CH704381A1 (de) * | 2011-01-24 | 2012-07-31 | Alstom Technology Ltd | Verfahren zum Betrieb eines Gasturbinenkraftwerks mit Abgasrezirkulation sowie Gasturbinenkraftwerk mit Abgasrezirkulation. |
US20130048097A1 (en) * | 2011-08-30 | 2013-02-28 | Firestar Engineering, Llc | Thermal phase separation |
FR2986229B1 (fr) * | 2012-01-27 | 2014-03-21 | Centre Nat Detudes Spatiales Cnes | Nouveaux monergols ioniques a base de n2o pour la propulsion spatiale |
WO2013116378A1 (en) | 2012-01-30 | 2013-08-08 | Firestar Engineering, Llc | Carbon-on-carbon manufacturing |
JP5908059B2 (ja) * | 2012-02-23 | 2016-04-26 | 昭和電工株式会社 | 発電装置、発電方法、分解ガスボイラー及び分解ガスタービン |
US9459059B2 (en) * | 2012-05-10 | 2016-10-04 | Peter John Hamilton | Mechanisms for firing projectiles and methods of their use |
US9334069B1 (en) * | 2012-10-23 | 2016-05-10 | The Boeing Company | Propellant gauging at microgravity within the pressure—temperature—density inflection zone of xenon |
WO2014116796A1 (en) * | 2013-01-23 | 2014-07-31 | Combustion 8 Technologies Llc | Increased diesel engine efficiency by using nitrous oxide as a fuel additive |
US9989014B2 (en) * | 2014-03-28 | 2018-06-05 | The Boeing Company | Premixed liquid propellant propulsion system and method with anti-flashback quenching liquid injector |
CN104035333B (zh) * | 2014-05-23 | 2015-06-10 | 北京空间飞行器总体设计部 | 一种深空探测器动力下降初始关键参数优化方法 |
JP6991542B2 (ja) * | 2016-03-23 | 2022-02-03 | 国立研究開発法人宇宙航空研究開発機構 | 噴射システム |
US10634094B2 (en) | 2016-05-27 | 2020-04-28 | The Boeing Company | Methods, systems and apparatuses for combustible lead for high triple point propellants |
US10934030B2 (en) * | 2016-07-21 | 2021-03-02 | The Boeing Company | Rocket propellant mixing and fueling systems and methods |
DE102018114868A1 (de) | 2018-06-20 | 2019-12-24 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Antriebssystem für ein Raumfahrzeug und Verfahren zum Antrieb eines Raumfahrzeugs |
DE102019123057A1 (de) | 2019-08-28 | 2021-03-04 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Antriebssystem für ein Raumfahrzeug und Verfahren zum Betreiben eines Raumfahrzeugs |
RU2740948C1 (ru) * | 2020-05-18 | 2021-01-21 | Андрей Валерьевич Шеленин | Экологическое топливо |
CN112177697B (zh) * | 2020-09-09 | 2022-02-22 | 西安交通大学 | 基于热分解反应的热防护耦合开式布雷顿发电系统 |
RU2761188C1 (ru) * | 2021-04-12 | 2021-12-06 | Андрей Валерьевич Шеленин | Ракетное топливо |
Family Cites Families (109)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1061847A (en) * | 1912-10-04 | 1913-05-13 | Alexander Constantine Ionides Jr | Means for preventing the backward propagation of flame. |
US1102653A (en) * | 1913-10-01 | 1914-07-07 | Robert H Goddard | Rocket apparatus. |
US1103503A (en) * | 1914-05-15 | 1914-07-14 | Robert H Goddard | Rocket apparatus. |
US1586195A (en) * | 1924-12-06 | 1926-05-25 | Standard Oil Co | Flame arrester |
US2447086A (en) * | 1944-01-15 | 1948-08-17 | Union Carbide & Carbon Corp | Backfire arrester and flash back preventer |
US2526222A (en) * | 1948-01-02 | 1950-10-17 | Daniel And Florence Guggenheim | Cooling and feeding means for rocket type combustion chambers |
US2609281A (en) * | 1948-09-25 | 1952-09-02 | Smith Welding Equipment Corp | Flashback arrester |
US2618540A (en) * | 1949-09-30 | 1952-11-18 | Air Reduction | Gas mixer |
LU31550A1 (ja) * | 1955-03-28 | |||
US3085393A (en) * | 1958-06-03 | 1963-04-16 | North American Aviation Inc | Rocket engine starting method |
US2960096A (en) * | 1959-08-24 | 1960-11-15 | Aqualite Corp | Preloaded rupturable-disc relief valve |
US3266241A (en) * | 1963-07-29 | 1966-08-16 | United Aircraft Corp | Propellant injector |
US3423272A (en) * | 1966-01-10 | 1969-01-21 | Hawkinson Paul E | Stitching machine and tire builder |
US3512556A (en) * | 1967-09-20 | 1970-05-19 | Serge N Mckhann | Self-protective conduit system |
US3535066A (en) * | 1968-08-26 | 1970-10-20 | Wagner Mining Scoop Inc | Flame arrester |
US3607369A (en) * | 1968-09-11 | 1971-09-21 | Union Carbide Corp | Method for forming porous aluminum layer |
US3719046A (en) * | 1970-07-02 | 1973-03-06 | Rocket Research Corp | Rocket engine cooling system |
US3748111A (en) * | 1971-06-11 | 1973-07-24 | W Klose | Flame arrestor |
US3730049A (en) * | 1971-06-25 | 1973-05-01 | Olin Corp | Safety system for explosive powder storage bin |
GB1399817A (en) * | 1971-11-08 | 1975-07-02 | Kidde & Co Walter | Pilot operated valve |
US3779714A (en) * | 1972-01-13 | 1973-12-18 | Scm Corp | Dispersion strengthening of metals by internal oxidation |
GB1407636A (en) * | 1972-11-28 | 1975-09-24 | Penny R N | Regenerative heat exchanger |
GB1520402A (en) * | 1974-07-30 | 1978-08-09 | Mitsubishi Electric Corp | Combustion apparatus |
JPS5627047A (en) * | 1979-08-07 | 1981-03-16 | Honda Motor Co Ltd | 4-cycle engine |
US4398527A (en) * | 1980-08-22 | 1983-08-16 | Chevron Research Company | Internal combustion engine having manifold and combustion surfaces coated with a foam |
US4446351A (en) * | 1981-02-27 | 1984-05-01 | Mitsubishi Denki Kabushiki Kaisha | Process for preparing a press die |
US4458595A (en) * | 1982-06-07 | 1984-07-10 | The United States Of America As Represented By The Secretary Of The Navy | Ablative liner |
JPS58214652A (ja) * | 1982-06-08 | 1983-12-13 | Natl Aerospace Lab | 複合冷却ロケツト燃焼器 |
US4673349A (en) * | 1984-12-20 | 1987-06-16 | Ngk Insulators, Ltd. | High temperature surface combustion burner |
US4707184A (en) * | 1985-05-31 | 1987-11-17 | Scm Metal Products, Inc. | Porous metal parts and method for making the same |
US4736676A (en) * | 1986-07-30 | 1988-04-12 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Composite piston |
GB8721018D0 (en) * | 1987-09-07 | 1987-10-14 | Alcan Int Ltd | Porous inorganic membrane support |
CA1312732C (en) * | 1987-10-21 | 1993-01-19 | John Eric Jackson | Fuel-oxidant mixture for detonation gun flame-plating |
US4902539A (en) * | 1987-10-21 | 1990-02-20 | Union Carbide Corporation | Fuel-oxidant mixture for detonation gun flame-plating |
US4992233A (en) * | 1988-07-15 | 1991-02-12 | Corning Incorporated | Sintering metal powders into structures without sintering aids |
US4909730A (en) * | 1989-01-23 | 1990-03-20 | Westech Industrial Ltd. | Flame arrester having detonation-attenuating means |
DE4135776C1 (ja) * | 1991-10-30 | 1993-05-06 | Dynamit Nobel Ag | |
US5203296A (en) * | 1992-04-09 | 1993-04-20 | Barbron Corporation | Flame arrester having helical flame arresting member |
US5305726A (en) * | 1992-09-30 | 1994-04-26 | United Technologies Corporation | Ceramic composite coating material |
DE4303169C1 (de) * | 1993-02-04 | 1994-04-28 | Dynamit Nobel Ag | Gasentwickelndes Material sowie Verwendung des Materials zur Erzeugung von Nutz- oder Druckgas |
US6003301A (en) * | 1993-04-14 | 1999-12-21 | Adroit Systems, Inc. | Exhaust nozzle for multi-tube detonative engines |
US5855827A (en) * | 1993-04-14 | 1999-01-05 | Adroit Systems, Inc. | Pulse detonation synthesis |
US5364586A (en) * | 1993-08-17 | 1994-11-15 | Ultram International L.L.C. | Process for the production of porous membranes |
US5477613A (en) * | 1993-12-21 | 1995-12-26 | United Technologies Corporation | Method of simultaneously forming rocket thrust chamber cooling tubes |
US5608179A (en) * | 1994-02-18 | 1997-03-04 | The United States Of America As Represented By The Administration Of The National Aeronautics And Space Administration | Catalytic ignitor for regenerative propellant gun |
US6652765B1 (en) * | 1994-11-30 | 2003-11-25 | Implant Innovations, Inc. | Implant surface preparation |
US6196164B1 (en) * | 1995-04-04 | 2001-03-06 | Srp 687 Pty. Ltd. | Ignition inhibiting gas water heater |
EP0752527B1 (en) * | 1995-07-06 | 2000-02-02 | Isuzu Ceramics Research Institute Co., Ltd. | Engine having sound absorption structures on the outer sides of combustion chambers |
US5632319A (en) * | 1995-10-04 | 1997-05-27 | Industrial Technology Research Institute | Method for manufacturing environmentally conscious foamed aluminum materials |
US5649720A (en) * | 1995-11-30 | 1997-07-22 | Morton International, Inc. | Inflators which store premixed fluid fuel and oxidizer in a porous matrix |
DE19621045C2 (de) * | 1996-05-24 | 1999-04-15 | Autoflator Ab | Gasgenerator |
US5768885A (en) * | 1996-12-03 | 1998-06-23 | Autoliv Asp, Inc. | Regenerative piston liquid propellant rocket motor |
JPH10175313A (ja) * | 1996-12-18 | 1998-06-30 | Tec Corp | インクジェットプリンタ |
US6098548A (en) * | 1997-03-05 | 2000-08-08 | Autoliv Asp, Inc. | Non-pyrotechnic initiator |
CA2572786A1 (en) * | 1997-04-04 | 1998-10-15 | University Of Southern California | Method for electrochemical fabrication including etching to remove flash |
DE19730674A1 (de) * | 1997-07-17 | 1999-01-21 | Deutsch Zentr Luft & Raumfahrt | Brennkammer und Verfahren zur Herstellung einer Brennkammer |
WO1999011832A1 (de) * | 1997-08-30 | 1999-03-11 | Honsel Ag | Legierung zum herstellen von metallschaumkörpern unter verwendung eines pulvers mit keimbildenden zusätzen |
US20060201178A1 (en) * | 1997-09-19 | 2006-09-14 | Smolko Daniel D | Cooling garment |
US6135070A (en) * | 1998-01-05 | 2000-10-24 | Robert A. Crandall | Two cycle 60 degree V6 and 90 degree V4 internal combustion engine |
US6397580B1 (en) * | 1998-07-09 | 2002-06-04 | Bi-Propellant Rocket Research Corporation | High performance rocket engine having a stepped expansion combustion chamber and method of making the same |
US6047541A (en) * | 1998-08-26 | 2000-04-11 | The United States Of America As Represented By The Secretary Of The Air Force | HAN TEAN (xm-46) mixing gas generator propellant tank pressurizer for launch vehicles and spacecraft |
US5925837A (en) * | 1998-09-16 | 1999-07-20 | Chien-Ping Ju | Manufacturing method and products of metallic friction material |
US6823831B2 (en) * | 1998-09-28 | 2004-11-30 | Parker-Hannifin Corporation | Flame arrestor system for fuel pump discharge |
US6045638A (en) * | 1998-10-09 | 2000-04-04 | Atlantic Research Corporation | Monopropellant and propellant compositions including mono and polyaminoguanidine dinitrate |
SE513930C2 (sv) * | 1999-02-26 | 2000-11-27 | Svenska Rymdaktiebolaget | Flytande drivmedel |
US6179608B1 (en) * | 1999-05-28 | 2001-01-30 | Precision Combustion, Inc. | Swirling flashback arrestor |
US6250072B1 (en) * | 1999-07-02 | 2001-06-26 | Quoin, Inc. | Multi-ignition controllable solid-propellant gas generator |
US6435211B2 (en) * | 1999-07-13 | 2002-08-20 | William L. Stone | HVAC damper |
US6984273B1 (en) * | 1999-07-29 | 2006-01-10 | Aerojet-General Corporation | Premixed liquid monopropellant solutions and mixtures |
AUPQ361299A0 (en) * | 1999-10-22 | 1999-11-18 | University Of Queensland, The | Reducing skin friction drag |
AU5695001A (en) * | 1999-11-11 | 2001-07-24 | Kelly Space & Technology, Inc. | Nitrous oxide/fuel monopropellants |
US6673173B1 (en) * | 2000-02-02 | 2004-01-06 | Autoliv Asp. Inc. | Gas generation with reduced NOx formation |
US6336318B1 (en) * | 2000-02-02 | 2002-01-08 | Hughes Electronics Corporation | Ion thruster having a hollow cathode assembly with an encapsulated heater, and its fabrication |
DE10034016C1 (de) * | 2000-07-13 | 2002-01-03 | Hilti Ag | Treibgas für brennkraftbetriebene Werkzeuge |
US6606851B1 (en) * | 2000-09-08 | 2003-08-19 | Joseph Roger Herdy, Jr. | Transpiration cooling of rocket engines |
US6779335B2 (en) * | 2000-12-07 | 2004-08-24 | Joseph Roger Herdy, Jr. | Burning nitrous oxide and a fuel |
US6915834B2 (en) * | 2001-02-01 | 2005-07-12 | Goldschmidt Ag | Process for producing metal foam and metal body produced using this process |
US6644961B2 (en) * | 2001-03-27 | 2003-11-11 | The Protectoseal Company | Flame arrestor with reflection suppressor |
US6719608B1 (en) * | 2001-04-19 | 2004-04-13 | Oluma, Inc. | Fabrication of devices with fibers engaged to grooves on substrates |
DE50212753D1 (de) * | 2001-07-26 | 2008-10-23 | Alstom Technology Ltd | Vormischbrenner mit hoher Flammenstabilität |
US6699035B2 (en) * | 2001-09-06 | 2004-03-02 | Enardo, Inc. | Detonation flame arrestor including a spiral wound wedge wire screen for gases having a low MESG |
US6896512B2 (en) * | 2001-09-19 | 2005-05-24 | Aztec Machinery Company | Radiator element |
US6755438B2 (en) * | 2001-10-22 | 2004-06-29 | Autoliv Asp, Inc. | Elongated inflator device and method of gas production |
AU2002364510A1 (en) * | 2001-12-05 | 2003-06-23 | Tda Research Inc. | Combustion process for synthesis of carbon nanomaterials from liquid hydrocarbon |
US6679049B2 (en) * | 2002-01-22 | 2004-01-20 | Hy Pat Corporation | Hybrid rocket motor having a precombustion chamber |
AU2003251395A1 (en) * | 2002-06-05 | 2003-12-22 | Faris, Sadeg, M. | Layered electrochemical cell and manufacturing method therefor |
CA2392687A1 (en) * | 2002-07-17 | 2004-01-17 | Antonio Miceli | Flashback precluding torch |
US6972064B2 (en) * | 2002-10-23 | 2005-12-06 | Alliant Techsystems Inc. | Method of forming laminar structures having variable angle tape wrap |
US20060121080A1 (en) * | 2002-11-13 | 2006-06-08 | Lye Whye K | Medical devices having nanoporous layers and methods for making the same |
US7597936B2 (en) * | 2002-11-26 | 2009-10-06 | University Of Utah Research Foundation | Method of producing a pigmented composite microporous material |
US7124574B2 (en) * | 2002-12-04 | 2006-10-24 | United Technologies Corporation | Method and apparatus for a substantially coaxial injector element |
US6799417B2 (en) * | 2003-02-05 | 2004-10-05 | Aerojet-General Corporation | Diversion of combustion gas within a rocket engine to preheat fuel |
US6931832B2 (en) * | 2003-05-13 | 2005-08-23 | United Technologies Corporation | Monopropellant combustion system |
US7757476B2 (en) * | 2003-07-22 | 2010-07-20 | The Aerospace Corporation | Catalytically activated transient decomposition propulsion system |
DE10336530B3 (de) * | 2003-08-05 | 2005-02-17 | Leinemann Gmbh & Co. | Flammendurchschlagsicherung |
US7585381B1 (en) * | 2003-08-07 | 2009-09-08 | Pioneer Astronautics | Nitrous oxide based explosives and methods for making same |
US6895743B1 (en) * | 2003-09-05 | 2005-05-24 | Mcelheran Terry | Liquid propellant rocket motor |
US7017329B2 (en) * | 2003-10-10 | 2006-03-28 | United Technologies Corporation | Method and apparatus for mixing substances |
US20050126755A1 (en) * | 2003-10-31 | 2005-06-16 | Berry Jonathan D. | Method and apparatus for improved flame stabilization |
US7569193B2 (en) * | 2003-12-19 | 2009-08-04 | Applied Materials, Inc. | Apparatus and method for controlled combustion of gaseous pollutants |
US7417714B2 (en) * | 2004-11-02 | 2008-08-26 | Nikon Corporation | Stage assembly with measurement system initialization, vibration compensation, low transmissibility, and lightweight fine stage |
US7451751B2 (en) * | 2004-12-10 | 2008-11-18 | Jim Atherley | Nitrous-oxide system |
US7370469B2 (en) * | 2004-12-13 | 2008-05-13 | United Technologies Corporation | Rocket chamber heat exchanger |
GR1005904B (el) * | 2005-10-31 | 2008-05-15 | ΑΡΙΣΤΟΤΕΛΕΙΟ ΠΑΝΕΠΙΣΤΗΜΙΟ ΘΕΣΣΑΛΟΝΙΚΗΣ-ΕΙΔΙΚΟΣ ΛΟΓΑΡΙΑΣΜΟΣ ΑΞΙΟΠΟΙΗΣΗΣ ΚΟΝΔΥΛΙΩΝ ΕΡΕΥΝΑΣ (κατά ποσοστό 40%) | Καταλυτικο φιλτρο μεταλλικου αφρου για το καυσαεριο των κινητηρων ντηζελ. |
US20070169461A1 (en) * | 2006-01-19 | 2007-07-26 | Honeywell International Inc. | Catalytic bipropellant hot gas generation system |
WO2008123895A2 (en) * | 2006-12-04 | 2008-10-16 | Firestar Engineering, Llc | Spark-integrated propellant injector head with flashback barrier |
US20090126514A1 (en) * | 2007-09-05 | 2009-05-21 | Eric Gregory Burroughs | Devices for collection and preparation of biological agents |
US20090071434A1 (en) * | 2007-09-19 | 2009-03-19 | Macmillan Shaun T | Low heat rejection high efficiency internal combustion engine |
US8671684B2 (en) * | 2008-04-16 | 2014-03-18 | Donald E. Moriarty | Partially self-refueling zero emissions system |
-
2008
- 2008-11-10 CN CN200880115398A patent/CN101855325A/zh active Pending
- 2008-11-10 EP EP08848086.8A patent/EP2209876A4/en not_active Withdrawn
- 2008-11-10 JP JP2010533326A patent/JP5711536B2/ja not_active Expired - Fee Related
- 2008-11-10 WO PCT/US2008/083039 patent/WO2009062183A1/en active Search and Examination
- 2008-11-10 AU AU2008323666A patent/AU2008323666A1/en not_active Abandoned
- 2008-11-10 US US12/268,266 patent/US20090133788A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
CN101855325A (zh) | 2010-10-06 |
EP2209876A1 (en) | 2010-07-28 |
EP2209876A4 (en) | 2014-01-08 |
WO2009062183A1 (en) | 2009-05-14 |
AU2008323666A1 (en) | 2009-05-14 |
JP2011502935A (ja) | 2011-01-27 |
US20090133788A1 (en) | 2009-05-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP5711536B2 (ja) | 一酸化二窒素と燃料とが混合されて成るモノプロペラント | |
Florczuk et al. | Performance evaluation of the hypergolic green propellants based on the HTP for a future next generation spacecrafts | |
Anflo et al. | Towards green propulsion for spacecraft with ADN-based monopropellants | |
Mayer et al. | European Fuel Blend development for in-space propulsion | |
Mungas et al. | NOFBX: A new non-toxic, Green propulsion technology with high performance and low cost | |
Surmacz | Green rocket propulsion research and development at the institute of aviation: problems and perspectives | |
Božić et al. | Program AHRES and its contribution to assess features and current limitations of hybrid rocket propulsion | |
Mishra et al. | Comparative study on propellant characteristics for reusable launch vehicles | |
Wilson et al. | Catalytic Decomposition of Nitrous Oxide Monopropellant for Hybrid Motor Re-Ignition | |
Chehroudi et al. | Liquid propellants and combustion: fundamentals and classifications | |
Wernimont | Monopropellant hydrogen peroxide rocket systems: optimum for small scale | |
Mehendiratta et al. | A review on different propellant materials for space vehicles and their characterisation | |
Colozza | Comparison of Mars aircraft propulsion systems | |
Zakirov | Investigation into nitrous oxide propulsion option for small satellite applications | |
Pinto et al. | Green gelled propellant highly throtteable rocket motor and gas generator technology: status and application | |
Shimada et al. | Study of low-cost 100kg-satellite launcher using hybrid rocket engines | |
Reed | On-board chemical propulsion technology | |
Kirchberger et al. | Green Propellants for Satellite Propulsion: Status of Research and Developments at DLR Lampoldshausen | |
Vozoff et al. | NOFBX: A Non-Toxic," Green" Propulsion Technology with High Performance and Low Cost | |
Anflo et al. | Development Testing of 1-Newton ADN-based rocket engines | |
AU2013273797A1 (en) | Nitrous oxide fuel blend monopropellants | |
SERCEL et al. | The ballistic Mars hopper-An alternative Mars mobility concept | |
Paravan et al. | Space Debris Mitigation and Remediation: Perspectives of Affordable Hybrid Propulsion Implementations | |
Ventura | Novel concepts for an advanced non-toxic gas generator | |
Tadini | Hybrid rocket propulsion for active removal of large abandoned objects |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20121030 |
|
A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20121130 |
|
A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20121207 |
|
A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20130212 |
|
A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20130219 |
|
A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20130423 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20140128 |
|
A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20140311 |
|
A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20140318 |
|
A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20140728 |
|
TRDD | Decision of grant or rejection written | ||
A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20150210 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20150306 |
|
R150 | Certificate of patent or registration of utility model |
Ref document number: 5711536 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
LAPS | Cancellation because of no payment of annual fees |