JPS6230296B2 - - Google Patents

Info

Publication number
JPS6230296B2
JPS6230296B2 JP53000352A JP35278A JPS6230296B2 JP S6230296 B2 JPS6230296 B2 JP S6230296B2 JP 53000352 A JP53000352 A JP 53000352A JP 35278 A JP35278 A JP 35278A JP S6230296 B2 JPS6230296 B2 JP S6230296B2
Authority
JP
Japan
Prior art keywords
diisocyanate
aziridine
liner
propellant
rocket motor
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.)
Expired
Application number
JP53000352A
Other languages
English (en)
Japanese (ja)
Other versions
JPS5388846A (en
Inventor
Dotsutoson Baado Jeemusu
Otsutoei Haitawaa Jeemusu
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ATK Launch Systems LLC
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 JPS5388846A publication Critical patent/JPS5388846A/ja
Publication of JPS6230296B2 publication Critical patent/JPS6230296B2/ja
Granted legal-status Critical Current

Links

Classifications

    • 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
    • C06B45/04Compositions 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
    • C06B45/06Compositions 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
    • C06B45/10Compositions 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
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G18/00Polymeric products of isocyanates or isothiocyanates
    • C08G18/06Polymeric products of isocyanates or isothiocyanates with compounds having active hydrogen
    • C08G18/28Polymeric products of isocyanates or isothiocyanates with compounds having active hydrogen characterised by the compounds used containing active hydrogen
    • C08G18/67Unsaturated compounds having active hydrogen
    • C08G18/69Polymers of conjugated dienes
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L19/00Compositions of rubbers not provided for in groups C08L7/00 - C08L17/00
    • C08L19/006Rubber characterised by functional groups, e.g. telechelic diene polymers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • F02K9/34Casings; Combustion chambers; Liners thereof
    • F02K9/346Liners, e.g. inhibitors

Landscapes

  • Chemical & Material Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Molecular Biology (AREA)
  • Dispersion Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Polyurethanes Or Polyureas (AREA)
  • Adhesives Or Adhesive Processes (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
JP35278A 1977-01-06 1978-01-05 Adhesive liner for caseebound solid propellant Granted JPS5388846A (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
JPS5388846A JPS5388846A (en) 1978-08-04
JPS6230296B2 true JPS6230296B2 (US20110009641A1-20110113-C00116.png) 1987-07-01

Family

ID=25047092

Family Applications (1)

Application Number Title Priority Date Filing Date
JP35278A Granted JPS5388846A (en) 1977-01-06 1978-01-05 Adhesive liner for caseebound solid propellant

Country Status (7)

Country Link
JP (1) JPS5388846A (US20110009641A1-20110113-C00116.png)
CA (1) CA1149174A (US20110009641A1-20110113-C00116.png)
DE (1) DE2758814A1 (US20110009641A1-20110113-C00116.png)
FR (1) FR2376833A1 (US20110009641A1-20110113-C00116.png)
GB (1) GB1585713A (US20110009641A1-20110113-C00116.png)
IL (1) IL53672A (US20110009641A1-20110113-C00116.png)
SE (1) SE439629B (US20110009641A1-20110113-C00116.png)

Families Citing this family (3)

* 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
GB2466512B (en) * 2008-12-23 2010-12-08 Adbruf Ltd A polymer and method of forming a polymer

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS52110752A (en) * 1976-01-16 1977-09-17 Canada Majesty In Right Of Curing binder compositions and method of using

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS52110752A (en) * 1976-01-16 1977-09-17 Canada Majesty In Right Of Curing binder compositions and method of using

Also Published As

Publication number Publication date
DE2758814A1 (de) 1978-07-13
JPS5388846A (en) 1978-08-04
IL53672A0 (en) 1978-03-10
CA1149174A (en) 1983-07-05
FR2376833B3 (US20110009641A1-20110113-C00116.png) 1980-09-26
GB1585713A (en) 1981-03-11
IL53672A (en) 1982-03-31
SE439629B (sv) 1985-06-24
SE7714556L (sv) 1978-07-07
FR2376833A1 (fr) 1978-08-04

Similar Documents

Publication Publication Date Title
US4429634A (en) Adhesive liner for case bonded solid propellant
US7011722B2 (en) Propellant formulation
US4163681A (en) Desensitized explosives and castable thermally stable high energy explosive compositions therefrom
JP6510641B2 (ja) Gap型バインダー中にadn装薬とrdx装薬とを有する複合火工製品及びその製造方法
JP2016064941A (ja) コンポジット推進薬用スラリー及びコンポジット推進薬
US4601862A (en) Delayed quick cure rocket motor liner
US3813308A (en) Case bonding system for cast composite propellants
US10889529B2 (en) Rocket motor propellants, systems and/or methods
US5872328A (en) Ferrocene derivatives
JPS6230296B2 (US20110009641A1-20110113-C00116.png)
US5031539A (en) Radiation curable rocket motor liner for case bonded solid propellant
US4427468A (en) Curable propellant binding systems with bonding agent combination
US3801385A (en) Processing aids for hydroxy-terminated polybutadiene propellant(u)
US3954701A (en) Polymer composition containing inorganic filler
US4736684A (en) Delayed quick cure rocket motor liner
US3745074A (en) Composite solid propellant with additive to improve the mechanical properties thereof
Kakade et al. Studies on interface properties of propellant liner for case-bonded composite propellants
US3762972A (en) Reaction product of phosphine oxide with carboxylic acids
US4747891A (en) Solid propellant containing an aziridinyl bonding agent
US4482408A (en) Plasticizer system for propellant compositions
CA1220627A (en) Thixotropic flame inhibitors for rocket propellant grains
US4375522A (en) Thixotropic restrictor, curable at room temperature, for use on solid propellant grains
US3532567A (en) Polyurethane propellant compositions prepared with hydroxy-terminated polyesters
JPS5941957B2 (ja) 複合発射薬製造用硬化性バインダ−組成物
US3809585A (en) Urethane propellant composition