GB1345257A - Jet propulsopm imots - Google Patents
Jet propulsopm imotsInfo
- Publication number
- GB1345257A GB1345257A GB2490971*A GB2490971A GB1345257A GB 1345257 A GB1345257 A GB 1345257A GB 2490971 A GB2490971 A GB 2490971A GB 1345257 A GB1345257 A GB 1345257A
- Authority
- GB
- United Kingdom
- Prior art keywords
- nozzle
- apertures
- thrust
- propulsopm
- imots
- 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
- 238000010276 construction Methods 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
- F02K9/97—Rocket nozzles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Processing Of Solid Wastes (AREA)
- Nozzles (AREA)
- Jet Pumps And Other Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19702022517 DE2022517A1 (de) | 1970-05-08 | 1970-05-08 | Raketentriebwerksduese mit Grenzschichtabsaugung |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1345257A true GB1345257A (en) | 1974-01-30 |
Family
ID=5770583
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2490971*A Expired GB1345257A (en) | 1970-05-08 | 1971-04-19 | Jet propulsopm imots |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3712546A (enExample) |
| DE (1) | DE2022517A1 (enExample) |
| FR (1) | FR2088412B3 (enExample) |
| GB (1) | GB1345257A (enExample) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2949522C2 (de) * | 1979-12-08 | 1982-01-28 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Gekühlte Schubdüse für ein Raketentriebwerk |
| FR2618488B1 (fr) * | 1987-07-20 | 1989-12-15 | Europ Propulsion | Divergent a rupture de galbe pour tuyere de moteur-fusee |
| US5619851A (en) * | 1989-02-08 | 1997-04-15 | United Technologies Corporation | Rocket nozzle for a rocket engine |
| US5683033A (en) * | 1989-02-08 | 1997-11-04 | United Technologies Corporation | Rocket nozzle for a rocket engine |
| DE3905748A1 (de) * | 1989-02-24 | 1993-06-03 | Dornier Gmbh | Scheinziel |
| WO2000032920A1 (en) * | 1998-11-27 | 2000-06-08 | Volvo Aero Corporation | Nozzle structure for rocket nozzles having cooled nozzle wall |
| SE516049C2 (sv) * | 2000-03-17 | 2001-11-12 | Volvo Aero Corp | Anordning för styrning av flödesseparationslinjen hos raketmunstycken |
| SE516046C2 (sv) | 2000-03-17 | 2001-11-12 | Volvo Aero Corp | Anordning för styrning av värmeöverföringen till munstycksväggen hos raketmotorer av expandertyp |
| GB2398046B (en) * | 2003-01-15 | 2006-07-12 | S & C Thermofluids Ltd | The use of porous surfaces with coanda effect |
| RU2551244C2 (ru) * | 2013-07-16 | 2015-05-20 | Федеральное государственное бюджетное учреждение науки Институт теоретической и прикладной механики им. С.А. Христиановича Сибирского отделения Российской академии наук (ИТПМ СО РАН) | Способ увеличения тяги сверхзвукового сопла ракетного двигателя |
| CN116696593A (zh) * | 2023-06-25 | 2023-09-05 | 哈尔滨工程大学 | 一种用于可渗透喷管的轻质多孔介质夹层结构 |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2481059A (en) * | 1944-08-28 | 1949-09-06 | Us Sec War | Adjustable rocket nozzle |
| FR1273933A (fr) * | 1960-09-06 | 1961-10-20 | Terseram Soc Nouv | Dispositif de sécurité pour tuyère de fusée |
| US3092963A (en) * | 1960-12-15 | 1963-06-11 | United Aircraft Corp | Vector control system |
| US3134224A (en) * | 1961-05-26 | 1964-05-26 | United Aircraft Corp | Gas bleed from rocket chamber |
| US3230705A (en) * | 1962-07-11 | 1966-01-25 | Trw Inc | Chemically cooled rocket |
| US3224678A (en) * | 1962-10-04 | 1965-12-21 | Marquardt Corp | Modular thrust chamber |
| US3297256A (en) * | 1965-07-08 | 1967-01-10 | Frederick R Hickerson | Thrust controlled rocket motor |
-
1970
- 1970-05-08 DE DE19702022517 patent/DE2022517A1/de active Pending
-
1971
- 1971-03-26 FR FR7110803A patent/FR2088412B3/fr not_active Expired
- 1971-04-19 GB GB2490971*A patent/GB1345257A/en not_active Expired
- 1971-05-03 US US00139397A patent/US3712546A/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| FR2088412A7 (enExample) | 1972-01-07 |
| FR2088412B3 (enExample) | 1973-12-28 |
| DE2022517A1 (de) | 1971-11-25 |
| US3712546A (en) | 1973-01-23 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed [section 19, patents act 1949] | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |