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GB984486A - Cellular synthetic resins suitable for incorporation in rocket motors - Google Patents

Cellular synthetic resins suitable for incorporation in rocket motors

Info

Publication number
GB984486A
GB984486A GB341863A GB341863A GB984486A GB 984486 A GB984486 A GB 984486A GB 341863 A GB341863 A GB 341863A GB 341863 A GB341863 A GB 341863A GB 984486 A GB984486 A GB 984486A
Authority
GB
United Kingdom
Prior art keywords
resin
thermosetting resin
incorporation
rocket
cured
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
GB341863A
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 GB984486A publication Critical patent/GB984486A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02K9/97Rocket nozzles
    • F02K9/974Nozzle- linings; Ablative coatings
    • 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

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Manufacture Of Porous Articles, And Recovery And Treatment Of Waste Products (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

A rocket combustion chamber is lined with a cured plastic composition containing microballoons embedded in a thermosetting resin. The composition is made by mixing a liquid thermosetting resin, e.g. an epoxy novalac, a curing agent, e.g. methyl bicyclo-[2,2,1]- 5 - heptene - 2,3 - dicarboxycylic anhydride, an accelerator for the curing reaction, e.g. tri-dimethylamino ethyl phenol or benzyldimethylamine and microballoons of silica glass or phenol-formaldehyde resin of 50 microns-0.125 inch diameter. A thickening agent, e.g. asbestos, cotton, wool, nylon or rayon fibres, may also be added. The mixture is heated to 160-200 DEG F. After application it is cured at 120-500 DEG F. Layers 12 and 19 of the resin may be applied to the rocket shell 11 by use of a polythene covered mandrel. An adhesive may also be used. Throat insert 13 may be made of molybdenum, tungsten, copper or aluminium and has a metallic oxide coating 14. Specification 917,627 is referred to. <PICT:0984486/C3/1>
GB341863A 1962-01-29 1963-01-28 Cellular synthetic resins suitable for incorporation in rocket motors Expired GB984486A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US16931962A 1962-01-29 1962-01-29

Publications (1)

Publication Number Publication Date
GB984486A true GB984486A (en) 1965-02-24

Family

ID=22615160

Family Applications (1)

Application Number Title Priority Date Filing Date
GB341863A Expired GB984486A (en) 1962-01-29 1963-01-28 Cellular synthetic resins suitable for incorporation in rocket motors

Country Status (3)

Country Link
CH (1) CH446814A (en)
DE (1) DE1235675B (en)
GB (1) GB984486A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3536656A (en) * 1966-02-21 1970-10-27 Gen Tire & Rubber Co Light-weight flexible insulating material
EP0822328A2 (en) * 1996-07-29 1998-02-04 Trw Inc. Throat insert for rocket thrusters

Families Citing this family (2)

* 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
DE10245741B4 (en) * 2002-10-01 2005-10-06 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Discharge nozzle for a solid rocket

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT182911B (en) * 1951-02-09 1955-08-25 Plansee Metallwerk Nozzle for jet propulsion (rockets)
GB759350A (en) * 1953-12-01 1956-10-17 English Electric Co Ltd Improvements in and relating to blast tubes
DE1069951B (en) * 1954-09-11 1959-11-26 The Carborundum Company, Niagara Fall's, N. Y. (V. St. A.) Device for burning fuel and for directed discharge of Verforeninuriigsgase, in particular for rocket engines
US2849860A (en) * 1955-10-17 1958-09-02 Norton Co Rocket motor with recrystallized silicon carbide throat insert
US2835107A (en) * 1956-12-21 1958-05-20 Haveg Industries Inc Resins and use thereof
DE1039787B (en) * 1957-06-08 1958-09-25 Ici Ltd Nozzles for engines with rocket propulsion
US3001362A (en) * 1957-07-26 1961-09-26 Russell Mfg Co Insulator for rocket motor
FR1281740A (en) * 1961-02-27 1962-01-12 Ici Ltd Expansion cone for the nozzle of a rocket engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3536656A (en) * 1966-02-21 1970-10-27 Gen Tire & Rubber Co Light-weight flexible insulating material
EP0822328A2 (en) * 1996-07-29 1998-02-04 Trw Inc. Throat insert for rocket thrusters
EP0822328A3 (en) * 1996-07-29 1999-10-20 Trw Inc. Throat insert for rocket thrusters

Also Published As

Publication number Publication date
DE1235675B (en) 1967-03-02
CH446814A (en) 1967-11-15

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