GB746214A - Improvements relating to rocket motors - Google Patents
Improvements relating to rocket motorsInfo
- Publication number
- GB746214A GB746214A GB14391/54A GB1439154A GB746214A GB 746214 A GB746214 A GB 746214A GB 14391/54 A GB14391/54 A GB 14391/54A GB 1439154 A GB1439154 A GB 1439154A GB 746214 A GB746214 A GB 746214A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lining
- insulating
- heat
- casing
- propellant
- 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
- 239000011810 insulating material Substances 0.000 abstract 2
- 239000003380 propellant Substances 0.000 abstract 2
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 abstract 1
- -1 ajuminium oxide Substances 0.000 abstract 1
- 239000004411 aluminium Substances 0.000 abstract 1
- 229910052782 aluminium Inorganic materials 0.000 abstract 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract 1
- 239000010425 asbestos Substances 0.000 abstract 1
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
- 229910052751 metal Inorganic materials 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
- 239000000203 mixture Substances 0.000 abstract 1
- 239000005011 phenolic resin Substances 0.000 abstract 1
- 229920001568 phenolic resin Polymers 0.000 abstract 1
- 229910052895 riebeckite Inorganic materials 0.000 abstract 1
- 238000005728 strengthening Methods 0.000 abstract 1
- 239000004753 textile Substances 0.000 abstract 1
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
- F02K9/08—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)
- Thermal Insulation (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE746214X | 1953-05-19 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB746214A true GB746214A (en) | 1956-03-14 |
Family
ID=20323228
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB14391/54A Expired GB746214A (en) | 1953-05-19 | 1954-05-17 | Improvements relating to rocket motors |
Country Status (3)
| Country | Link |
|---|---|
| BE (1) | BE528963A (https=) |
| FR (1) | FR1100712A (https=) |
| GB (1) | GB746214A (https=) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3010355A (en) * | 1957-06-10 | 1961-11-28 | Phillips Petroleum Co | Method for making a rocket motor |
| US3017744A (en) * | 1957-07-11 | 1962-01-23 | James A Jett | Propellant grain and rocket motor |
| US3077734A (en) * | 1956-12-10 | 1963-02-19 | Phillips Petroleum Co | Solid-propellant rocket motor |
| US3235183A (en) * | 1963-05-29 | 1966-02-15 | United Aircraft Corp | Ablation cooled rocket nozzle |
| DE1214476B (de) * | 1956-12-21 | 1966-04-14 | Haveg Industries Inc | Hochtemperaturfestes Bau- bzw. Schutzschicht-material fuer Raketenbrennkammern oder Flugkoerperaussenhuellen |
| US3301785A (en) * | 1960-05-02 | 1967-01-31 | North American Aviation Inc | Insulated solid propellant rocket motor |
| US5280706A (en) * | 1992-06-25 | 1994-01-25 | Thiokol Corporation | Composite/metal hybrid rocket motor case and methods for manufacturing |
| US5564272A (en) * | 1994-07-29 | 1996-10-15 | Thiokol Corporation | Slotted hybrid pressure vessel |
| RU2304726C2 (ru) * | 2005-09-28 | 2007-08-20 | Открытое акционерное общество "Институт прикладной физики" | Корпус ракетного двигателя на твердом топливе |
| RU2831320C2 (ru) * | 2005-09-28 | 2024-12-04 | Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации | Корпус ракетного двигателя на твердом топливе |
-
0
- BE BE528963D patent/BE528963A/xx unknown
-
1954
- 1954-05-17 FR FR1100712D patent/FR1100712A/fr not_active Expired
- 1954-05-17 GB GB14391/54A patent/GB746214A/en not_active Expired
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3077734A (en) * | 1956-12-10 | 1963-02-19 | Phillips Petroleum Co | Solid-propellant rocket motor |
| DE1214476B (de) * | 1956-12-21 | 1966-04-14 | Haveg Industries Inc | Hochtemperaturfestes Bau- bzw. Schutzschicht-material fuer Raketenbrennkammern oder Flugkoerperaussenhuellen |
| US3010355A (en) * | 1957-06-10 | 1961-11-28 | Phillips Petroleum Co | Method for making a rocket motor |
| US3017744A (en) * | 1957-07-11 | 1962-01-23 | James A Jett | Propellant grain and rocket motor |
| US3301785A (en) * | 1960-05-02 | 1967-01-31 | North American Aviation Inc | Insulated solid propellant rocket motor |
| US3235183A (en) * | 1963-05-29 | 1966-02-15 | United Aircraft Corp | Ablation cooled rocket nozzle |
| US5280706A (en) * | 1992-06-25 | 1994-01-25 | Thiokol Corporation | Composite/metal hybrid rocket motor case and methods for manufacturing |
| US5348603A (en) * | 1992-06-25 | 1994-09-20 | Thiokol Corporation | Composite/metal hybrid rocket motor case and methods for manufacturing |
| US5564272A (en) * | 1994-07-29 | 1996-10-15 | Thiokol Corporation | Slotted hybrid pressure vessel |
| RU2304726C2 (ru) * | 2005-09-28 | 2007-08-20 | Открытое акционерное общество "Институт прикладной физики" | Корпус ракетного двигателя на твердом топливе |
| RU2418186C2 (ru) * | 2005-09-28 | 2011-05-10 | Виктор Фридрихович Ланг | Корпус ракетного двигателя на твердом топливе |
| RU2831320C2 (ru) * | 2005-09-28 | 2024-12-04 | Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации | Корпус ракетного двигателя на твердом топливе |
Also Published As
| Publication number | Publication date |
|---|---|
| BE528963A (https=) | |
| FR1100712A (fr) | 1955-09-23 |
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