GB984486A - Cellular synthetic resins suitable for incorporation in rocket motors - Google Patents
Cellular synthetic resins suitable for incorporation in rocket motorsInfo
- 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
Links
Classifications
-
- 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
- F02K9/97—Rocket nozzles
- F02K9/974—Nozzle- linings; Ablative coatings
-
- 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
- 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>
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)
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)
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)
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 |
-
1963
- 1963-01-28 GB GB341863A patent/GB984486A/en not_active Expired
- 1963-01-29 DE DE1963T0023400 patent/DE1235675B/en active Pending
- 1963-01-29 CH CH111763A patent/CH446814A/en unknown
Cited By (3)
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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