WO2010061127A3 - Composite composition for solid propellants including a ferrocene derivative and a submicronic aluminum charge, solid propellant, and load - Google Patents

Composite composition for solid propellants including a ferrocene derivative and a submicronic aluminum charge, solid propellant, and load Download PDF

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Publication number
WO2010061127A3
WO2010061127A3 PCT/FR2009/052285 FR2009052285W WO2010061127A3 WO 2010061127 A3 WO2010061127 A3 WO 2010061127A3 FR 2009052285 W FR2009052285 W FR 2009052285W WO 2010061127 A3 WO2010061127 A3 WO 2010061127A3
Authority
WO
WIPO (PCT)
Prior art keywords
solid
submicronic
load
ferrocene derivative
composite composition
Prior art date
Application number
PCT/FR2009/052285
Other languages
French (fr)
Other versions
WO2010061127A2 (en
Inventor
Hélène BLANCHARD
Christian Perut
Original Assignee
Snpe Materiaux Energetiques
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Snpe Materiaux Energetiques filed Critical Snpe Materiaux Energetiques
Priority to EP09797078A priority Critical patent/EP2349953A2/en
Priority to CN2009801464763A priority patent/CN102256915A/en
Publication of WO2010061127A2 publication Critical patent/WO2010061127A2/en
Publication of WO2010061127A3 publication Critical patent/WO2010061127A3/en
Priority to IL212794A priority patent/IL212794A0/en

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B23/00—Compositions characterised by non-explosive or non-thermic constituents
    • C06B23/007—Ballistic modifiers, burning rate catalysts, burning rate depressing agents, e.g. for gas generating
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B23/00—Compositions characterised by non-explosive or non-thermic constituents
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B33/00—Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide
    • C06B33/06—Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide the material being an inorganic oxygen-halogen salt
    • 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
    • C06B45/04—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive
    • C06B45/06—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive the solid solution or matrix containing an organic component
    • C06B45/10—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive the solid solution or matrix containing an organic component the organic component containing a resin

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Health & Medical Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Inorganic Chemistry (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Dispersion Chemistry (AREA)
  • Molecular Biology (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Catalysts (AREA)
  • Medicinal Preparation (AREA)
  • Solid Fuels And Fuel-Associated Substances (AREA)

Abstract

The present invention relates to composite compositions for solid propellants including an oxidizing charge, a liquid polyol polymer, a combustion catalyst consisting of a ferrocene derivative, and an aluminum charge. Said aluminum charge is characteristically submicronic, or even nanometric. The present invention also relates to pasty or solid propellant, and to the corresponding solid propellant loads.
PCT/FR2009/052285 2008-11-25 2009-11-24 Composite composition for solid propellants including a ferrocene derivative and a submicronic aluminum charge, solid propellant, and load WO2010061127A2 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP09797078A EP2349953A2 (en) 2008-11-25 2009-11-24 Composite composition for solid propellants including a ferrocene derivative and a submicronic aluminum charge, solid propellant, and load
CN2009801464763A CN102256915A (en) 2008-11-25 2009-11-24 Composite composition for solid propellants including a ferrocene derivative and a submicronic aluminum charge, solid propellant, and load
IL212794A IL212794A0 (en) 2008-11-25 2011-05-09 Composite composition for solid propellants including a ferrocene derivative and a submicronic aluminum charge, solid propellant, and load

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0858001A FR2938837B1 (en) 2008-11-25 2008-11-25 COMPOSITE COMPOSITION FOR SOLID PROPERGOL COMPRISING A FERROCENIC DERIVATIVE AND A SUBMICRONIC ALUMINUM LOAD, SOLID PROPERGOL AND LOADING
FR0858001 2008-11-25

Publications (2)

Publication Number Publication Date
WO2010061127A2 WO2010061127A2 (en) 2010-06-03
WO2010061127A3 true WO2010061127A3 (en) 2010-07-29

Family

ID=41112496

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2009/052285 WO2010061127A2 (en) 2008-11-25 2009-11-24 Composite composition for solid propellants including a ferrocene derivative and a submicronic aluminum charge, solid propellant, and load

Country Status (6)

Country Link
EP (1) EP2349953A2 (en)
KR (1) KR20110110131A (en)
CN (1) CN102256915A (en)
FR (1) FR2938837B1 (en)
IL (1) IL212794A0 (en)
WO (1) WO2010061127A2 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2474567C2 (en) * 2010-07-21 2013-02-10 Государственное образовательное учреждение высшего профессионального образования Томский государственный университет (ТГУ) Method of producing mixed solid fuel with metal fuel
CA2867258C (en) * 2012-03-12 2020-07-14 University Of Central Florida Research Foundation, Inc. Compositions having aluminum particles dispersed in a continuous phase
CN102641748B (en) * 2012-04-24 2014-04-30 中国地质大学（武汉） Preparation method of hydroxyl burning-rate catalyst for substituent ferrocenylsilanes grafting and product thereof
FR3007758B1 (en) * 2013-06-28 2015-10-09 Herakles COMPOSITE SOLID PROPERGOL WHOSE ALUMINUM REDUCTIVE LOAD HAS A LOW MAGNESIUM LEVEL
US10196324B2 (en) * 2014-12-08 2019-02-05 Raytheon Company Ferrocenyl bonding agent oxidizers
CN105642880B (en) * 2016-01-25 2018-02-13 中北大学 It is a kind of to contain energy cavity liner using micro-nano thermite as material

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3932240A (en) * 1973-06-04 1976-01-13 The United States Of America As Represented By The Secretary Of The Navy Burning rate modifying binder for propellant and method
US4302258A (en) * 1978-11-06 1981-11-24 Nissan Motor Company, Limited Composite propellant with 0.2μ or smaller metal fuel
US4411717A (en) * 1983-02-02 1983-10-25 The United States Of America As Represented By The Secretary Of The Air Force Solid rocket propellants comprising guignet's green pigment
EP0794192A1 (en) * 1996-03-06 1997-09-10 Chemische Betriebe Pluto GmbH Ferrocene derivatives

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3932240A (en) * 1973-06-04 1976-01-13 The United States Of America As Represented By The Secretary Of The Navy Burning rate modifying binder for propellant and method
US4302258A (en) * 1978-11-06 1981-11-24 Nissan Motor Company, Limited Composite propellant with 0.2μ or smaller metal fuel
US4411717A (en) * 1983-02-02 1983-10-25 The United States Of America As Represented By The Secretary Of The Air Force Solid rocket propellants comprising guignet's green pigment
EP0794192A1 (en) * 1996-03-06 1997-09-10 Chemische Betriebe Pluto GmbH Ferrocene derivatives

Non-Patent Citations (7)

* Cited by examiner, † Cited by third party
Title
41ST AIAA/ASME/SAE/ASEE JOINT PROPULSION CONFERENCE AND EXHIBIT - 41ST AIAA/ASME/SAE/ASEE JOINT PROPULSION CONFERENCE AND EXHIBIT 2005 AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS INC. USA, 2005 *
DATABASE CA [online] CHEMICAL ABSTRACTS SERVICE, COLUMBUS, OHIO, US; 2004, LI, FENG-SHENG ET AL: "Catalytic effect of nanometer metal powders on the thermal decomposition of AP and AP/HTPB solid propellant", XP002549112, retrieved from STN Database accession no. 144:90558 *
DATABASE COMPENDEX [online] ENGINEERING INFORMATION, INC., NEW YORK, NY, US; 2005, SHALOM A ET AL: "The effect of nanosized aluminum on composite propellant properties", XP002549113, Database accession no. E20093612283914 *
GALFETTI, L. ET AL: "Nanoparticles for solid rocket propulsion", JOURNAL OF PHYSICS: CONDENSED MATTER , 18(33), S1991-S2005 CODEN: JCOMEL; ISSN: 0953-8984, 2006, XP002549110 *
GALFETTI, L. ET AL: "Pre and post - burning analysis of nano aluminized solid rocket propellants", AEROSPACE SCIENCE AND TECHNOLOGY , 11(1), 26-32 CODEN: ARSTFZ; ISSN: 1270-9638, 2007, XP002549111 *
GUO ET AL: "Preparation and reactivity of aluminum nanopowders coated by hydroxyl-terminated polybutadiene (HTPB)", APPLIED SURFACE SCIENCE, ELSEVIER, AMSTERDAM, NL, vol. 254, no. 8, 1 February 2008 (2008-02-01), pages 2413 - 2417, XP022449372, ISSN: 0169-4332 *
HANNENG CAILIAO , 12(SUPPL. 1), 253-256 CODEN: HACAFQ; ISSN: 1006-9941, 2004 *

Also Published As

Publication number Publication date
KR20110110131A (en) 2011-10-06
EP2349953A2 (en) 2011-08-03
FR2938837A1 (en) 2010-05-28
WO2010061127A2 (en) 2010-06-03
FR2938837B1 (en) 2011-05-06
IL212794A0 (en) 2011-07-31
CN102256915A (en) 2011-11-23

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