FR2093469A5 - - Google Patents
Info
- Publication number
- FR2093469A5 FR2093469A5 FR7116176A FR7116176A FR2093469A5 FR 2093469 A5 FR2093469 A5 FR 2093469A5 FR 7116176 A FR7116176 A FR 7116176A FR 7116176 A FR7116176 A FR 7116176A FR 2093469 A5 FR2093469 A5 FR 2093469A5
- Authority
- FR
- France
- 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
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B47/00—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase
- C06B47/02—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase the components comprising a binary propellant
- C06B47/08—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase the components comprising a binary propellant a component containing hydrazine or a hydrazine derivative
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US3585870A | 1970-05-08 | 1970-05-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2093469A5 true FR2093469A5 (fr) | 1972-01-28 |
Family
ID=21885215
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7116176A Expired FR2093469A5 (fr) | 1970-05-08 | 1971-05-05 |
Country Status (3)
Country | Link |
---|---|
US (1) | US3695041A (fr) |
DE (1) | DE2122742A1 (fr) |
FR (1) | FR2093469A5 (fr) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3871828A (en) * | 1972-10-10 | 1975-03-18 | Hughes Aircraft Co | Hydrazine gas generator |
US3903693A (en) * | 1973-03-26 | 1975-09-09 | Anthony Fox | Rocket motor housing |
US4069664A (en) * | 1974-01-24 | 1978-01-24 | Hughes Aircraft Company | Monopropellant thruster |
US4324096A (en) * | 1979-04-23 | 1982-04-13 | Hughes Aircraft Company | Hydrazine thruster |
US4856271A (en) * | 1987-10-01 | 1989-08-15 | Olin Corporation | Gas generator and generating method employing dual catalytic and thermal liquid propellant decomposition paths |
US5711695A (en) * | 1995-05-01 | 1998-01-27 | Pitsco, Inc. | Gas-propelled toy with exhaust nozzle for gas cartridge |
US6860099B1 (en) * | 2003-01-09 | 2005-03-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Liquid propellant tracing impingement injector |
US6918243B2 (en) * | 2003-05-19 | 2005-07-19 | The Boeing Company | Bi-propellant injector with flame-holding zone igniter |
US7827781B2 (en) * | 2005-12-05 | 2010-11-09 | Bendel Timothy B | Liquid propellant rocket engine with pintle injector and acoustic dampening |
US8122703B2 (en) | 2006-04-28 | 2012-02-28 | United Technologies Corporation | Coaxial ignition assembly |
US20130199155A1 (en) * | 2012-01-02 | 2013-08-08 | Jordin Kare | Rocket Propulsion Systems, and Related Methods |
US20140182265A1 (en) * | 2013-01-03 | 2014-07-03 | Jordin Kare | Rocket Propulsion Systems, and Related Methods |
US11661907B2 (en) | 2018-10-11 | 2023-05-30 | Sierra Space Corporation | Vortex hybrid rocket motor |
US20210148307A1 (en) | 2019-01-30 | 2021-05-20 | 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 |
US20220120240A1 (en) * | 2020-10-16 | 2022-04-21 | Sierra Nevada Corporation | Vortex thruster system including catalyst bed with screen assembly |
US11952967B2 (en) | 2021-08-19 | 2024-04-09 | Sierra Space Corporation | Liquid propellant injector for vortex hybrid rocket motor |
US20230191351A1 (en) * | 2021-12-21 | 2023-06-22 | Firehawk Aerospace, Inc. | Catalytic decomposition reactors |
US11879414B2 (en) | 2022-04-12 | 2024-01-23 | Sierra Space Corporation | Hybrid rocket oxidizer flow control system including regression rate sensors |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2706887A (en) * | 1946-01-23 | 1955-04-26 | Harlow B Grow | Liquid propellant rocket motor |
GB851448A (en) * | 1957-06-21 | 1960-10-19 | Armstrong Siddeley Motors Ltd | Improvements in and relating to combustion chambers |
US3107485A (en) * | 1959-05-27 | 1963-10-22 | Ohio Commw Eng Co | Propulsion means and method for space vehicles employing a volatile alkene and metalcarbonyl |
US3149460A (en) * | 1960-09-28 | 1964-09-22 | Gen Electric | Reaction propulsion system |
US3377140A (en) * | 1965-10-15 | 1968-04-09 | Specialties Dev Corp | Apparatus for catalytically decomposing hydrazine |
US3446023A (en) * | 1966-08-05 | 1969-05-27 | United Aircraft Corp | Catalytic attitude-control rocket motor |
-
1970
- 1970-05-08 US US35858A patent/US3695041A/en not_active Expired - Lifetime
-
1971
- 1971-05-05 FR FR7116176A patent/FR2093469A5/fr not_active Expired
- 1971-05-07 DE DE19712122742 patent/DE2122742A1/de active Pending
Also Published As
Publication number | Publication date |
---|---|
US3695041A (en) | 1972-10-03 |
DE2122742A1 (de) | 1971-12-02 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |