JP2005528469A - 極低温の単一系固体燃料の製造方法および該方法に従って製造された固体燃料 - Google Patents
極低温の単一系固体燃料の製造方法および該方法に従って製造された固体燃料 Download PDFInfo
- Publication number
- JP2005528469A JP2005528469A JP2003583976A JP2003583976A JP2005528469A JP 2005528469 A JP2005528469 A JP 2005528469A JP 2003583976 A JP2003583976 A JP 2003583976A JP 2003583976 A JP2003583976 A JP 2003583976A JP 2005528469 A JP2005528469 A JP 2005528469A
- Authority
- JP
- Japan
- Prior art keywords
- solid
- liquid
- fuel
- phase
- sponges
- 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
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Classifications
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- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/402—Propellant tanks; Feeding propellants
-
- 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
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/403—Solid propellant rocket engines
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Crystallography & Structural Chemistry (AREA)
- Solid Fuels And Fuel-Associated Substances (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Manufacture Of Porous Articles, And Recovery And Treatment Of Waste Products (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP02090144A EP1354862A1 (de) | 2002-04-16 | 2002-04-16 | Verfahren zum Herstellen von kryogenen, monergolen Festtreibstoffen und danach erzeugte Festtreibstoffe |
| PCT/EP2003/003860 WO2003087017A1 (de) | 2002-04-16 | 2003-04-14 | Verfahren zum herstellen von kryogenen, monergolen festtreibstoffen und danach erzeugte festtreibstoffe |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2005528469A true JP2005528469A (ja) | 2005-09-22 |
| JP2005528469A5 JP2005528469A5 (https=) | 2009-09-10 |
Family
ID=28459559
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2003583976A Pending JP2005528469A (ja) | 2002-04-16 | 2003-04-14 | 極低温の単一系固体燃料の製造方法および該方法に従って製造された固体燃料 |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US8147628B2 (https=) |
| EP (1) | EP1354862A1 (https=) |
| JP (1) | JP2005528469A (https=) |
| CN (1) | CN100337995C (https=) |
| AU (1) | AU2003229662A1 (https=) |
| IL (1) | IL164566A0 (https=) |
| RU (1) | RU2312847C2 (https=) |
| WO (1) | WO2003087017A1 (https=) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1354862A1 (de) | 2002-04-16 | 2003-10-22 | Lo, Roger E. | Verfahren zum Herstellen von kryogenen, monergolen Festtreibstoffen und danach erzeugte Festtreibstoffe |
| FR2915479B1 (fr) * | 2007-04-26 | 2009-08-21 | Snpe Materiaux Energetiques Sa | Gel pyrotechnique ; propergol solide ; chargement pyrotechnique ; procedes d'obtention |
| EP1992675A1 (de) * | 2007-05-10 | 2008-11-19 | BAUER Maschinen GmbH | Brennstoffkomponente für einen Explosivstoff sowie Verfahren zu dessen Herstellung |
| CN101338236B (zh) * | 2008-08-12 | 2012-02-22 | 浙江大学 | 一种含聚二茂铁基化合物燃速促进剂的推进剂及其制备方法 |
| CN103254025B (zh) * | 2013-04-26 | 2015-10-28 | 西安近代化学研究所 | 一种高燃烧性能铝粉组合物及其制备方法 |
| CN103333036B (zh) * | 2013-06-21 | 2016-06-29 | 宜宾北方川安化工有限公司 | 一种低临界压力双基推进剂 |
| WO2015176307A1 (zh) * | 2014-05-23 | 2015-11-26 | 天津大学 | 一种自燃液体推进剂组合物 |
| CN106518583B (zh) * | 2016-10-27 | 2017-11-14 | 中国人民解放军国防科学技术大学 | 一种米级超高燃速高能致密复合材料及其制备方法 |
| CN107824791B (zh) * | 2017-11-24 | 2019-09-03 | 中国工程物理研究院激光聚变研究中心 | 一种泡沫铍材料的制备方法 |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3137127A (en) * | 1961-03-28 | 1964-06-16 | Res Inst Of Temple University | Method of developing high energy thrust |
| US3191535A (en) * | 1959-05-25 | 1965-06-29 | Dow Chemical Co | Solid cellular metallic propellants |
| US3259532A (en) * | 1963-07-24 | 1966-07-05 | Reynolds Metals Co | Combustion system comprising sponge metal, liquid oxygen, and finely divided carbon |
| US3687746A (en) * | 1959-06-16 | 1972-08-29 | Exxon Research Engineering Co | Rocket propellant system |
| US6101808A (en) * | 1998-05-29 | 2000-08-15 | Orbital Technologies Corporation | Cryogenic solid hybrid rocket engine and method of propelling a rocket |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3367268A (en) * | 1959-10-05 | 1968-02-06 | Exxon Research Engineering Co | Hybrid rocket propellent grain |
| US3143446A (en) * | 1959-11-27 | 1964-08-04 | Gen Electric | Propellant charge containing fluid encapsulations |
| US3204560A (en) * | 1961-04-24 | 1965-09-07 | Lockheed Aircraft Corp | Solid rocket propellant containing metal encapsulated gas |
| US3691769A (en) * | 1964-01-16 | 1972-09-19 | United Aircraft Corp | Multi-component propellant jet propulsion |
| US3367286A (en) * | 1965-09-01 | 1968-02-06 | Steinthal & Co Inc M | Load control systems |
| US5834539A (en) * | 1991-10-15 | 1998-11-10 | Krivohlavek; Dennis | Multiple phase emulsions in burner fuel, combustion, emulsion and explosives applications |
| US5529648A (en) * | 1993-12-23 | 1996-06-25 | Aerodyne Research, Inc. | Heterogeneous fuel for hybrid rocket |
| EP1354862A1 (de) | 2002-04-16 | 2003-10-22 | Lo, Roger E. | Verfahren zum Herstellen von kryogenen, monergolen Festtreibstoffen und danach erzeugte Festtreibstoffe |
-
2002
- 2002-04-16 EP EP02090144A patent/EP1354862A1/de not_active Withdrawn
-
2003
- 2003-04-14 AU AU2003229662A patent/AU2003229662A1/en not_active Abandoned
- 2003-04-14 WO PCT/EP2003/003860 patent/WO2003087017A1/de not_active Ceased
- 2003-04-14 JP JP2003583976A patent/JP2005528469A/ja active Pending
- 2003-04-14 RU RU2004133348/02A patent/RU2312847C2/ru active
- 2003-04-14 CN CNB038111772A patent/CN100337995C/zh not_active Expired - Fee Related
- 2003-04-14 US US10/511,865 patent/US8147628B2/en not_active Expired - Fee Related
-
2004
- 2004-10-13 IL IL16456604A patent/IL164566A0/xx unknown
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3191535A (en) * | 1959-05-25 | 1965-06-29 | Dow Chemical Co | Solid cellular metallic propellants |
| US3687746A (en) * | 1959-06-16 | 1972-08-29 | Exxon Research Engineering Co | Rocket propellant system |
| US3137127A (en) * | 1961-03-28 | 1964-06-16 | Res Inst Of Temple University | Method of developing high energy thrust |
| US3259532A (en) * | 1963-07-24 | 1966-07-05 | Reynolds Metals Co | Combustion system comprising sponge metal, liquid oxygen, and finely divided carbon |
| US6101808A (en) * | 1998-05-29 | 2000-08-15 | Orbital Technologies Corporation | Cryogenic solid hybrid rocket engine and method of propelling a rocket |
Also Published As
| Publication number | Publication date |
|---|---|
| US8147628B2 (en) | 2012-04-03 |
| WO2003087017A1 (de) | 2003-10-23 |
| CN1653018A (zh) | 2005-08-10 |
| AU2003229662A1 (en) | 2003-10-27 |
| RU2312847C2 (ru) | 2007-12-20 |
| US20050189051A1 (en) | 2005-09-01 |
| CN100337995C (zh) | 2007-09-19 |
| RU2004133348A (ru) | 2005-08-20 |
| EP1354862A1 (de) | 2003-10-22 |
| IL164566A0 (en) | 2005-12-18 |
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