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 PDF

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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
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solid
liquid
fuel
phase
sponges
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JP2005528469A5 (https=
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ロ・ロジャー・エー
アディリム・ハリィ
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    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00Compositions or products which are defined by structure or arrangement of component of product
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/402Propellant tanks; Feeding propellants
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B47/00Compositions 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
    • C06B47/02Compositions 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
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06DMEANS FOR GENERATING SMOKE OR MIST; GAS-ATTACK COMPOSITIONS; GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART)
    • C06D5/00Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/403Solid propellant rocket engines

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  • 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)
JP2003583976A 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 Pending JP2005528469A (ja)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (5)

* Cited by examiner, † Cited by third party
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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