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 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/en
Publication of IL53672A publication Critical patent/IL53672A/en

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)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Dispersion Chemistry (AREA)
  • Molecular Biology (AREA)
  • Crystallography & Structural Chemistry (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 (en)
CA (1) CA1149174A (en)
DE (1) DE2758814A1 (en)
FR (1) FR2376833A1 (en)
GB (1) GB1585713A (en)
IL (1) IL53672A (en)
SE (1) SE439629B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3105932C2 (en) * 1981-02-18 1982-12-02 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Insulating layer for propellants
DE3644239A1 (en) * 1986-12-23 1988-07-07 Bayern Chemie Gmbh Flugchemie INTERMEDIATE LAYER BETWEEN THE DRIVELINE AND THE INSULATION LAYER OF A ROCKET SOLID DRIVE KIT
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
FR2376833A1 (en) 1978-08-04
JPS5388846A (en) 1978-08-04
CA1149174A (en) 1983-07-05
GB1585713A (en) 1981-03-11
SE7714556L (en) 1978-07-07
DE2758814A1 (en) 1978-07-13
SE439629B (en) 1985-06-24
JPS6230296B2 (en) 1987-07-01
IL53672A0 (en) 1978-03-10
FR2376833B3 (en) 1980-09-26

Similar Documents

Publication Publication Date Title
PH11334A (en) Nitroparaffin explosive composition
GB2055358B (en) Emulsion-type explosive composition and method for the preparation thereof
ZW6679A1 (en) Blasting explosives composition
JPS52118800A (en) Igniter for rocket motor
DE3376863D1 (en) Weather seal arrangement for solid rocket motor igniters
JPS5767097A (en) Nitramine composite propellant composition
IL53672A (en) Method for bonding solid propellant grain to rocket motor casing and polymeric composition therefor
ZA756345B (en) Nitroparaffin explosive composition
GB2049891B (en) Solid propellant rocket motor
JPS55144496A (en) Manufacture of nooflash pressed rocket propellant
GB2228731B (en) Autopyrolysable propellant composition
JPS5650196A (en) Solid propellant
DE3066145D1 (en) Cap-sensitive powdered explosive composition
GB2033410B (en) Polyurethane compositions for rocket casing liners
GB2097377B (en) Double-base solid propellent material
GB8408437D0 (en) Propellant for rocket
JPS5491695A (en) Digital servo motor
EG11915A (en) Improvements in or relating to the casting of rocket motor propellants
PL239744A1 (en) Hard deflagrating nitroglycerine explosive
IT8049955A0 (en) ROCKET PROPELLANT COMPOSITION AND ROCKET USING SAID COMPOSITION
GB2265695B (en) Improvements in or relating to rocket motors
CA899628A (en) Priming composition for propellant charges and rocket propellant grains
JPS5792590A (en) Composite propellant composition
JPS5551791A (en) Delayyaction explosive composition
EG11616A (en) Improvements relating to propellant charges

Legal Events

Date Code Title Description
KB Patent renewed