IL51941A - Solid propellant with finely divided aluminum oxide as burning rate catalyst - Google Patents

Solid propellant with finely divided aluminum oxide as burning rate catalyst

Info

Publication number
IL51941A
IL51941A IL51941A IL5194177A IL51941A IL 51941 A IL51941 A IL 51941A IL 51941 A IL51941 A IL 51941A IL 5194177 A IL5194177 A IL 5194177A IL 51941 A IL51941 A IL 51941A
Authority
IL
Israel
Prior art keywords
aluminum oxide
finely divided
solid propellant
burning rate
divided aluminum
Prior art date
Application number
IL51941A
Other languages
English (en)
Original Assignee
Thiokol Corp
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 Thiokol Corp filed Critical Thiokol Corp
Publication of IL51941A publication Critical patent/IL51941A/xx

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
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S149/00—Explosive and thermic compositions or charges
    • Y10S149/11—Particle size of a component

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Dispersion Chemistry (AREA)
  • Molecular Biology (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Catalysts (AREA)
  • Solid Fuels And Fuel-Associated Substances (AREA)
  • Medicinal Preparation (AREA)
  • Agricultural Chemicals And Associated Chemicals (AREA)
IL51941A 1976-04-22 1977-04-26 Solid propellant with finely divided aluminum oxide as burning rate catalyst IL51941A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/679,101 US4084992A (en) 1976-04-22 1976-04-22 Solid propellant with alumina burning rate catalyst

Publications (1)

Publication Number Publication Date
IL51941A true IL51941A (en) 1982-04-30

Family

ID=24725559

Family Applications (1)

Application Number Title Priority Date Filing Date
IL51941A IL51941A (en) 1976-04-22 1977-04-26 Solid propellant with finely divided aluminum oxide as burning rate catalyst

Country Status (8)

Country Link
US (1) US4084992A (sv)
JP (1) JPS6028797B2 (sv)
CA (1) CA1090581A (sv)
DE (1) DE2718013A1 (sv)
FR (1) FR2360537A1 (sv)
GB (1) GB1542620A (sv)
IL (1) IL51941A (sv)
SE (1) SE440223B (sv)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4158583A (en) * 1977-12-16 1979-06-19 Nasa High performance ammonium nitrate propellant
GB2193491B (en) * 1978-07-21 1988-09-14 Imi Kynoch Limited Kynoch Work Improvements in propellants
US4375522A (en) * 1980-07-21 1983-03-01 The United States Of America As Represented By The Secretary Of The Navy Thixotropic restrictor, curable at room temperature, for use on solid propellant grains
US5334270A (en) * 1992-01-29 1994-08-02 Thiokol Corporation Controlled burn rate, reduced smoke, solid propellant formulations
US5771679A (en) * 1992-01-29 1998-06-30 Thiokol Corporation Aluminized plateau-burning solid propellant formulations and methods for their use
CA2115557C (en) * 1992-07-13 2000-07-25 Tadao Yoshida Air bag gas generating composition
US5470408A (en) * 1993-10-22 1995-11-28 Thiokol Corporation Use of carbon fibrils to enhance burn rate of pyrotechnics and gas generants
US6740180B1 (en) * 1997-07-15 2004-05-25 Anthony Joseph Cesaroni Thermoplastic polymer propellant compositions
US6086692A (en) * 1997-10-03 2000-07-11 Cordant Technologies, Inc. Advanced designs for high pressure, high performance solid propellant rocket motors
AU1449199A (en) * 1997-10-03 1999-04-27 Cordant Technologies, Inc. High pressure, high performance solid rocket hydroxy-terminated polybutadiene propellant formulations
US6217682B1 (en) * 1997-10-27 2001-04-17 Cordant Technologies Inc. Energetic oxetane propellants
CN105017050A (zh) * 2015-07-14 2015-11-04 西安近代化学研究所 左旋多巴铅化合物及其制备方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3822154A (en) * 1962-10-01 1974-07-02 Aerojet General Co Suppression of unstable burning using finely divided metal oxides
US3310946A (en) * 1965-10-05 1967-03-28 Richard A Dobbins Method for minimizing combustion instability
US3924405A (en) * 1973-06-07 1975-12-09 Aerojet General Co Solid propellants with stability enhanced additives of particulate refractory carbides or oxides
US3986906A (en) * 1974-12-23 1976-10-19 The United States Of America As Represented By The Secretary Of The Army Ultrahigh burning rate propellants containing an organic perchlorate oxidizer

Also Published As

Publication number Publication date
FR2360537B3 (sv) 1980-03-07
GB1542620A (en) 1979-03-21
DE2718013A1 (de) 1977-11-17
FR2360537A1 (fr) 1978-03-03
SE7704691L (sv) 1977-10-23
SE440223B (sv) 1985-07-22
CA1090581A (en) 1980-12-02
JPS6028797B2 (ja) 1985-07-06
DE2718013C2 (sv) 1987-06-19
US4084992A (en) 1978-04-18
JPS52145508A (en) 1977-12-03

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