CH463879A - Générateur de gaz chauds - Google Patents
Générateur de gaz chaudsInfo
- Publication number
- CH463879A CH463879A CH951362A CH951362A CH463879A CH 463879 A CH463879 A CH 463879A CH 951362 A CH951362 A CH 951362A CH 951362 A CH951362 A CH 951362A CH 463879 A CH463879 A CH 463879A
- Authority
- CH
- Switzerland
- Prior art keywords
- gas generator
- hot gas
- hot
- generator
- gas
- Prior art date
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
- F02K9/72—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nitrogen Condensed Heterocyclic Rings (AREA)
- Feeding And Controlling Fuel (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
- Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR871893A FR1311203A (fr) | 1961-08-30 | 1961-08-30 | Perfectionnements apportés aux générateurs de gaz chauds, notamment aux moteursfusées, à propergol liquide-solide de caractère hypergolique |
FR903830A FR82456E (fr) | 1961-08-30 | 1962-07-12 | Perfectionnements apportés aux générateurs de gaz chauds, notamment aux moteursfusées, à propergol liquide-solide de caractère hypergolique |
Publications (1)
Publication Number | Publication Date |
---|---|
CH463879A true CH463879A (fr) | 1968-10-15 |
Family
ID=26192079
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH951362A CH463879A (fr) | 1961-08-30 | 1962-08-09 | Générateur de gaz chauds |
Country Status (5)
Country | Link |
---|---|
US (1) | US3315472A (fr) |
CH (1) | CH463879A (fr) |
DE (4) | DE1237383B (fr) |
FR (2) | FR1311203A (fr) |
GB (1) | GB1010453A (fr) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3456440A (en) * | 1966-11-09 | 1969-07-22 | Northrop Corp | Gas generating system |
US3397540A (en) * | 1966-12-12 | 1968-08-20 | Army Usa | Hybrid rocket motor having turbulator-mixer apparatus |
US3423943A (en) * | 1967-02-27 | 1969-01-28 | Us Navy | Hybrid rocket motor |
US3677011A (en) * | 1969-01-22 | 1972-07-18 | Us Air Force | Thrust control system for hybrid rocket motors |
US3908358A (en) * | 1973-01-31 | 1975-09-30 | Thiokol Corp | Variable flow gas generating method and system |
US4744300A (en) * | 1984-09-25 | 1988-05-17 | Diehl Gmbh & Co. | Utilization of metal hydride and acidic reagent for the accelerating of masses and propulsion devices for applying such materials |
US4765134A (en) * | 1986-08-28 | 1988-08-23 | United Technologies Corporation | Acoustic oscillatory pressure control for solid propellant rocket |
GB2291478B (en) * | 1990-03-26 | 1996-07-10 | Marconi Co Ltd | Lithium-water reactor |
US5133183A (en) * | 1991-03-01 | 1992-07-28 | The United States Of America As Represented By The Secretary Of The Army | Gel/solid bipropellant propulsion system with energy management capability |
US6014857A (en) * | 1996-12-05 | 2000-01-18 | Stinnesbeck; Thomas L. | High fuel regression hybrid rocket motor |
FR2844557B1 (fr) * | 2002-09-12 | 2006-03-03 | Snecma Propulsion Solide | Systeme et procede de controle des oscillations de pression d'origine hydrodynamique pour propulseur a propergol solide |
US8350199B2 (en) * | 2009-01-13 | 2013-01-08 | The Boeing Company | Apparatus to reduce thrust oscillations in a launch vehicle |
IT1403760B1 (it) * | 2011-01-07 | 2013-10-31 | Hypotheses Srl | Camere di combustione con presenza di vorticatori e sistemi di iniezione injectorless per motori ibridi |
US9273635B2 (en) * | 2012-03-29 | 2016-03-01 | The Aerospace Corporation | Hypergolic hybrid motor igniter |
CN102943719B (zh) * | 2012-11-06 | 2015-02-25 | 北京航空航天大学 | 固液火箭发动机后燃室扰流装置 |
RU2656073C1 (ru) * | 2016-12-12 | 2018-05-30 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" | Способ дросселирования тяги жидкостного ракетного двигателя |
US11661907B2 (en) * | 2018-10-11 | 2023-05-30 | Sierra Space Corporation | Vortex hybrid rocket motor |
WO2020154809A1 (fr) * | 2019-01-30 | 2020-08-06 | Laboratoire Reaction Dynamics Inc. | Moteurs-fusées |
US12060853B2 (en) | 2019-01-30 | 2024-08-13 | Laboratoire Reaction Dynamics Inc. | Rocket engine with integrated oxidizer catalyst in manifold and injector assembly |
US11572851B2 (en) | 2019-06-21 | 2023-02-07 | Sierra Space Corporation | Reaction control vortex thruster system |
US11952967B2 (en) | 2021-08-19 | 2024-04-09 | Sierra Space Corporation | Liquid propellant injector for vortex hybrid rocket motor |
US11879414B2 (en) | 2022-04-12 | 2024-01-23 | Sierra Space Corporation | Hybrid rocket oxidizer flow control system including regression rate sensors |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE21756C (de) * | C. WALDER in Berlin SW., Grofsbeerenstr. 92 | Schlittschuhbefestigung | ||
GB570210A (en) * | 1942-11-06 | 1945-06-27 | James Taylor | Improvements in gas-escape reaction-propelled devices |
US2990682A (en) * | 1951-11-07 | 1961-07-04 | Gen Electric | Fuel charge |
US3068641A (en) * | 1955-04-18 | 1962-12-18 | Homer M Fox | Hybrid method of rocket propulsion |
US3093960A (en) * | 1959-04-20 | 1963-06-18 | Olin Mathieson | Method of producing thrust by reacting a metal azide with a boron and hydrogen containing compound |
US3159104A (en) * | 1959-11-02 | 1964-12-01 | Solid Fuels Corp | Laminated tape propellants |
US3144751A (en) * | 1961-05-10 | 1964-08-18 | United Aircraft Corp | Hybrid rocket |
US3173251A (en) * | 1962-03-16 | 1965-03-16 | Jr Harrison Allen | Apparatus for igniting solid propellants |
US3142152A (en) * | 1962-06-22 | 1964-07-28 | Lockheed Aircraft Corp | Hybrid rocket motor |
-
1961
- 1961-08-30 FR FR871893A patent/FR1311203A/fr not_active Expired
-
1962
- 1962-07-12 FR FR903830A patent/FR82456E/fr not_active Expired
- 1962-07-31 GB GB2931?/62A patent/GB1010453A/en not_active Expired
- 1962-08-02 DE DEO11337A patent/DE1237383B/de active Pending
- 1962-08-02 DE DEO11338A patent/DE1237843B/de active Pending
- 1962-08-02 DE DEO8902A patent/DE1237841B/de active Pending
- 1962-08-02 DE DEO11336A patent/DE1237842B/de active Pending
- 1962-08-09 CH CH951362A patent/CH463879A/fr unknown
-
1965
- 1965-10-13 US US495603A patent/US3315472A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FR82456E (fr) | 1964-02-21 |
DE1237383B (de) | 1967-03-23 |
DE1237841B (de) | 1967-03-30 |
US3315472A (en) | 1967-04-25 |
DE1237842B (de) | 1967-03-30 |
FR1311203A (fr) | 1962-12-07 |
DE1237843B (de) | 1967-03-30 |
GB1010453A (en) | 1965-11-17 |
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