IL53672A - Method for bonding solid propellant grain to rocket motor casing and polymeric composition therefor - Google Patents

Method for bonding solid propellant grain to rocket motor casing and polymeric composition therefor

Info

Publication number
IL53672A
IL53672A IL53672A IL5367277A IL53672A IL 53672 A IL53672 A IL 53672A IL 53672 A IL53672 A IL 53672A IL 5367277 A IL5367277 A IL 5367277A IL 53672 A IL53672 A IL 53672A
Authority
IL
Israel
Prior art keywords
polymeric composition
motor casing
rocket motor
solid propellant
propellant grain
Prior art date
Application number
IL53672A
Other languages
English (en)
Other versions
IL53672A0 (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 IL53672A0 publication Critical patent/IL53672A0/xx
Publication of IL53672A publication Critical patent/IL53672A/xx

Links

Classifications

    • 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
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G18/00—Polymeric products of isocyanates or isothiocyanates
    • C08G18/06—Polymeric products of isocyanates or isothiocyanates with compounds having active hydrogen
    • C08G18/28—Polymeric products of isocyanates or isothiocyanates with compounds having active hydrogen characterised by the compounds used containing active hydrogen
    • C08G18/67—Unsaturated compounds having active hydrogen
    • C08G18/69—Polymers of conjugated dienes
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L19/00—Compositions of rubbers not provided for in groups C08L7/00 - C08L17/00
    • C08L19/006—Rubber characterised by functional groups, e.g. telechelic diene polymers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F02K9/346—Liners, e.g. inhibitors

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • Organic Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Medicinal Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Molecular Biology (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Dispersion Chemistry (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Polyurethanes Or Polyureas (AREA)
  • Adhesives Or Adhesive Processes (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
IL53672A 1977-01-06 1977-12-21 Method for bonding solid propellant grain to rocket motor casing and polymeric composition therefor IL53672A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US75726077A 1977-01-06 1977-01-06

Publications (2)

Publication Number Publication Date
IL53672A0 IL53672A0 (en) 1978-03-10
IL53672A true IL53672A (en) 1982-03-31

Family

ID=25047092

Family Applications (1)

Application Number Title Priority Date Filing Date
IL53672A IL53672A (en) 1977-01-06 1977-12-21 Method for bonding solid propellant grain to rocket motor casing and polymeric composition therefor

Country Status (7)

Country Link
JP (1) JPS5388846A (enrdf_load_stackoverflow)
CA (1) CA1149174A (enrdf_load_stackoverflow)
DE (1) DE2758814A1 (enrdf_load_stackoverflow)
FR (1) FR2376833A1 (enrdf_load_stackoverflow)
GB (1) GB1585713A (enrdf_load_stackoverflow)
IL (1) IL53672A (enrdf_load_stackoverflow)
SE (1) SE439629B (enrdf_load_stackoverflow)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3105932C2 (de) * 1981-02-18 1982-12-02 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Isolierschicht für Treibsätze
DE3644239A1 (de) * 1986-12-23 1988-07-07 Bayern Chemie Gmbh Flugchemie Zwischenschicht zwischen dem treibsatz und der isolierschicht eines raketenfeststoff-treibsatzes
RU2212395C1 (ru) * 2002-02-20 2003-09-20 Федеральный центр двойных технологий "Союз" Способ изготовления зарядов смесевого ракетного твердого топлива
GB2466512B (en) * 2008-12-23 2010-12-08 Adbruf Ltd A polymer and method of forming a polymer

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1056984A (en) * 1976-01-16 1979-06-19 Her Majesty The Queen In Right Of Canada As Represented By The Minister Of National Defence Of Her Majesty's Canadian Government Curable binding systems

Also Published As

Publication number Publication date
JPS5388846A (en) 1978-08-04
CA1149174A (en) 1983-07-05
FR2376833B3 (enrdf_load_stackoverflow) 1980-09-26
JPS6230296B2 (enrdf_load_stackoverflow) 1987-07-01
DE2758814A1 (de) 1978-07-13
SE7714556L (sv) 1978-07-07
FR2376833A1 (fr) 1978-08-04
GB1585713A (en) 1981-03-11
IL53672A0 (en) 1978-03-10
SE439629B (sv) 1985-06-24

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Legal Events

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