DE68900273D1 - Zweistoffraketenmotor. - Google Patents
Zweistoffraketenmotor.Info
- Publication number
- DE68900273D1 DE68900273D1 DE8989304763T DE68900273T DE68900273D1 DE 68900273 D1 DE68900273 D1 DE 68900273D1 DE 8989304763 T DE8989304763 T DE 8989304763T DE 68900273 T DE68900273 T DE 68900273T DE 68900273 D1 DE68900273 D1 DE 68900273D1
- Authority
- DE
- Germany
- Prior art keywords
- rocket engine
- fuel rocket
- fuel
- engine
- rocket
- 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 - Fee Related
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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/52—Injectors
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB888811126A GB8811126D0 (en) | 1988-05-11 | 1988-05-11 | Bipropellant rocket engines |
Publications (1)
Publication Number | Publication Date |
---|---|
DE68900273D1 true DE68900273D1 (de) | 1991-10-24 |
Family
ID=10636710
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8989304763T Expired - Fee Related DE68900273D1 (de) | 1988-05-11 | 1989-05-10 | Zweistoffraketenmotor. |
Country Status (5)
Country | Link |
---|---|
US (1) | US4894986A (de) |
EP (1) | EP0342023B1 (de) |
JP (1) | JP2812710B2 (de) |
DE (1) | DE68900273D1 (de) |
GB (1) | GB8811126D0 (de) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5805973A (en) * | 1991-03-25 | 1998-09-08 | General Electric Company | Coated articles and method for the prevention of fuel thermal degradation deposits |
US5891584A (en) * | 1991-03-25 | 1999-04-06 | General Electric Company | Coated article for hot hydrocarbon fluid and method of preventing fuel thermal degradation deposits |
US5873241A (en) * | 1991-05-23 | 1999-02-23 | United Technologies Corporation | Rocket engine auxiliary power system |
US5427507A (en) * | 1992-06-19 | 1995-06-27 | Regents Of The University Of California | Valving for controlling a fluid-driven reciprocating apparatus |
US5222873A (en) * | 1992-06-19 | 1993-06-29 | The United States Of America As Represented By The United States Department Of Energy | Fluid-driven reciprocating apparatus and valving for controlling same |
US5247792A (en) * | 1992-07-27 | 1993-09-28 | General Electric Company | Reducing thermal deposits in propulsion systems |
US5616005A (en) * | 1994-11-08 | 1997-04-01 | Regents Of The University Of California | Fluid driven recipricating apparatus |
RU2158841C2 (ru) | 1999-01-21 | 2000-11-10 | Открытое акционерное общество "НПО Энергомаш им. акад. В.П. Глушко" | Камера жидкостного ракетного двигателя и ее корпус |
DE19958310C2 (de) * | 1999-12-03 | 2002-01-17 | Daimler Chrysler Ag | Raketentriebwerk für Flüssigtreibstoffe mit einem geschlossenen Triebwerkskreislauf |
US6918243B2 (en) * | 2003-05-19 | 2005-07-19 | The Boeing Company | Bi-propellant injector with flame-holding zone igniter |
DE10353423B3 (de) * | 2003-11-15 | 2005-04-14 | Eads Space Transportation Gmbh | Einspritzelement |
US7503511B2 (en) * | 2004-09-08 | 2009-03-17 | Space Exploration Technologies | Pintle injector tip with active cooling |
US8122703B2 (en) | 2006-04-28 | 2012-02-28 | United Technologies Corporation | Coaxial ignition assembly |
KR100674118B1 (ko) * | 2006-07-07 | 2007-01-24 | (주)씨앤스페이스 | 로켓 추진용 메탄엔진 |
US7784268B1 (en) * | 2006-08-04 | 2010-08-31 | Xcor Aerospace | Partial superheat cycle for operating a pump in a rocket system |
US7958719B2 (en) * | 2007-03-28 | 2011-06-14 | The Aerospace Corporation | Noncircular transient fluid fuel injector control channels in propellant injector combustion systems |
US7762058B2 (en) * | 2007-04-17 | 2010-07-27 | Pratt & Whitney Rocketdyne, Inc. | Ultra-compact, high performance aerovortical rocket thruster |
US7690192B2 (en) * | 2007-04-17 | 2010-04-06 | Pratt & Whitney Rocketdyne, Inc. | Compact, high performance swirl combustion rocket engine |
US9404441B2 (en) * | 2008-08-18 | 2016-08-02 | Aerojet Rocketdyne Of De, Inc. | Low velocity injector manifold for hypergolic rocket engine |
US8727284B2 (en) * | 2010-01-22 | 2014-05-20 | Hamilton Sundstrand Corporation | Turbine powered electromechanical actuation system |
US11181076B2 (en) | 2016-03-03 | 2021-11-23 | Kevin Michael Weldon | Rocket engine bipropellant supply system including an electrolyzer |
EP3829979A4 (de) | 2018-05-25 | 2022-05-18 | Radian Aerospace, Inc. | Transportsystem von erde zu umlaufbahn |
WO2020010098A1 (en) * | 2018-07-03 | 2020-01-09 | Radian Aerospace, Inc. | Rocket propulsion systems and associated methods |
WO2020050689A1 (ko) * | 2018-09-06 | 2020-03-12 | 페리지항공우주 주식회사 | 액체 추진제 로켓 엔진의 추진장치 |
DE102021109484A1 (de) * | 2021-04-15 | 2022-10-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Triebwerkseinheit für einen Raketenantrieb und Brennkammervorrichtung |
US20230012171A1 (en) * | 2021-07-06 | 2023-01-12 | AT Space Pty Ltd | Propellant injector for hybrid rocket engines |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2667740A (en) * | 1950-06-06 | 1954-02-02 | Daniel And Florence Guggenheim | Means for supplying and cooling rocket type combustion chambers |
US3040520A (en) * | 1954-11-22 | 1962-06-26 | Garrett Corp | Jet power unit for an aircraft |
US2962858A (en) * | 1956-11-23 | 1960-12-06 | Aficano Alfred | Fuel injection apparatus |
GB853495A (en) * | 1957-09-13 | 1960-11-09 | Allan Barker British | Improvements in or relating to liquid propellent rocket motors |
US3257799A (en) * | 1963-02-01 | 1966-06-28 | United Aircraft Corp | Method for aeration of liquid propellants |
DE1257489B (de) * | 1965-05-15 | 1967-12-28 | Boelkow Gmbh | Raketentriebwerk fuer fluessige Treibstoffe mit einer Hauptbrennkammer und einer Vorbrennkammer |
GB1167948A (en) * | 1967-06-03 | 1969-10-22 | Rolls Royce | Rocket Engine. |
US3534909A (en) * | 1968-05-21 | 1970-10-20 | Paine Thomas O | Control valve and co-axial variable injector |
US3712059A (en) * | 1970-12-03 | 1973-01-23 | Textron Inc | Reverse flow internally-cooled rocket engine |
US3722219A (en) * | 1971-04-26 | 1973-03-27 | Us Navy | Variable area injector for rocket engine |
JPS59181928U (ja) * | 1983-05-18 | 1984-12-04 | 株式会社日立製作所 | 低カロリ−ガス用燃料ノズル |
DE3328117A1 (de) * | 1983-08-04 | 1985-02-14 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Verfahren zum betreiben eines nebenstrom-raketentriebwerkes |
US4771599A (en) * | 1986-10-20 | 1988-09-20 | United Technologies Corporation | Tripropellant rocket engine with injector |
-
1988
- 1988-05-11 GB GB888811126A patent/GB8811126D0/en active Pending
-
1989
- 1989-04-26 US US07/343,444 patent/US4894986A/en not_active Expired - Fee Related
- 1989-05-10 DE DE8989304763T patent/DE68900273D1/de not_active Expired - Fee Related
- 1989-05-10 JP JP1117168A patent/JP2812710B2/ja not_active Expired - Lifetime
- 1989-05-10 EP EP89304763A patent/EP0342023B1/de not_active Expired
Also Published As
Publication number | Publication date |
---|---|
EP0342023B1 (de) | 1991-09-18 |
JPH01318752A (ja) | 1989-12-25 |
US4894986A (en) | 1990-01-23 |
EP0342023A1 (de) | 1989-11-15 |
JP2812710B2 (ja) | 1998-10-22 |
GB8811126D0 (en) | 1988-12-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE68900273D1 (de) | Zweistoffraketenmotor. | |
DE68912214D1 (de) | Motorregler. | |
DE68908321T2 (de) | Mantelgebläse-Turbinentriebwerk. | |
DE3866137D1 (de) | Sonnenbetriebener stirling-motor. | |
DE68908734D1 (de) | Schalldämpfer. | |
DE3761916D1 (de) | Raketentriebwerke. | |
DE68911510D1 (de) | Wärmegedämpfter motor. | |
NO885677L (no) | Ammunisjon. | |
DE68903201T2 (de) | Waermeisolierte brennkraftmaschine. | |
DE68905997T2 (de) | Brennkraftmaschinenblock. | |
DE68903944D1 (de) | Raketenwerfer. | |
DE3860912D1 (de) | Einspritzbrennkraftmaschine. | |
DE58901928D1 (de) | Kurbelwelle. | |
DE68904207T2 (de) | Zuendsystem. | |
DE58906566D1 (de) | Aufgebaute Kurbelwelle. | |
DE69002215D1 (de) | Raketenbrennkammer. | |
DE68901253D1 (de) | Anlasser. | |
DE58904491D1 (de) | Viertakt-brennkraftmaschine. | |
DE59000083D1 (de) | Turbostrahltriebwerk. | |
DE58906750D1 (de) | Geräuschdämpfer. | |
DE59101352D1 (de) | Raketenmotor. | |
DE68905748T2 (de) | Brennraum. | |
DE68904869D1 (de) | Vergaserzusammenbau. | |
FR2686409B1 (fr) | Projectile supersonique pilotable. | |
DE3861284D1 (de) | Verbrennungsmotor. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |