JPH0452859B2 - - Google Patents
Info
- Publication number
- JPH0452859B2 JPH0452859B2 JP4050786A JP4050786A JPH0452859B2 JP H0452859 B2 JPH0452859 B2 JP H0452859B2 JP 4050786 A JP4050786 A JP 4050786A JP 4050786 A JP4050786 A JP 4050786A JP H0452859 B2 JPH0452859 B2 JP H0452859B2
- Authority
- JP
- Japan
- Prior art keywords
- combustion chamber
- hydrogen
- propulsion
- operating
- 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
- 238000002485 combustion reaction Methods 0.000 claims description 48
- 239000007789 gas Substances 0.000 claims description 36
- 239000001257 hydrogen Substances 0.000 claims description 32
- 229910052739 hydrogen Inorganic materials 0.000 claims description 32
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 24
- 239000003380 propellant Substances 0.000 claims description 21
- 238000000034 method Methods 0.000 claims description 16
- 230000007246 mechanism Effects 0.000 claims description 15
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 13
- 239000001301 oxygen Substances 0.000 claims description 13
- 229910052760 oxygen Inorganic materials 0.000 claims description 13
- 239000007788 liquid Substances 0.000 claims description 11
- 150000002431 hydrogen Chemical class 0.000 claims description 8
- 239000000567 combustion gas Substances 0.000 claims description 6
- 238000011144 upstream manufacturing Methods 0.000 claims description 3
- 238000002347 injection Methods 0.000 description 13
- 239000007924 injection Substances 0.000 description 13
- 238000001816 cooling Methods 0.000 description 3
- 239000000446 fuel Substances 0.000 description 3
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 206010067482 No adverse event Diseases 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000011017 operating method Methods 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000008207 working material Substances 0.000 description 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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/46—Feeding propellants using pumps
- F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19853506826 DE3506826A1 (de) | 1985-02-27 | 1985-02-27 | Verfahren zum betreiben eines fluessigkeitsraketentriebwerks und raketentriebwerk zur durchfuehrung des verfahrens |
DE3506826.4 | 1985-02-27 |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS61201871A JPS61201871A (ja) | 1986-09-06 |
JPH0452859B2 true JPH0452859B2 (ru) | 1992-08-25 |
Family
ID=6263649
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP4050786A Granted JPS61201871A (ja) | 1985-02-27 | 1986-02-27 | 液体ロケツトを作動させるための方法およびこの方法を実施するためのロケツト推進機構 |
Country Status (3)
Country | Link |
---|---|
JP (1) | JPS61201871A (ru) |
DE (1) | DE3506826A1 (ru) |
FR (1) | FR2577996B1 (ru) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0823336B2 (ja) * | 1987-10-06 | 1996-03-06 | 科学技術庁航空宇宙技術研究所長 | 推進剤加熱部を有するエンジン |
JPH0751942Y2 (ja) * | 1992-09-29 | 1995-11-29 | 株式会社大井製作所 | シートスライド装置 |
FR2698914B1 (fr) * | 1992-12-09 | 1995-03-03 | Europ Propulsion | Moteur-fusée à ergols liquides à flux dérivé et générateur de gaz intégré. |
US5918460A (en) * | 1997-05-05 | 1999-07-06 | United Technologies Corporation | Liquid oxygen gasifying system for rocket engines |
RU2158839C2 (ru) * | 1999-01-21 | 2000-11-10 | Открытое акционерное общество "НПО Энергомаш им. акад. В.П. Глушко" | Жидкостный ракетный двигатель с дожиганием турбогаза |
RU2155273C1 (ru) * | 1999-08-18 | 2000-08-27 | Открытое акционерное общество "НПО Энергомаш им.акад. В.П. Глушко" | Жидкостный ракетный двигатель (жрд) на криогенном топливе с замкнутым контуром привода турбины турбонасосного агрегата (варианты) |
DE10141108B4 (de) * | 2001-08-22 | 2005-06-30 | Eads Space Transportation Gmbh | Raketentriebwerk mit geschlossenen Triebwerkskreislauf mit modularer Zuführung der Turbinenabgase |
RU2447311C2 (ru) * | 2008-09-17 | 2012-04-10 | Владислав Сергеевич Буриков | Способ работы и устройство реактивного двигателя (варианты) |
US20120204535A1 (en) * | 2011-02-15 | 2012-08-16 | Pratt & Whitney Rocketdyne, Inc. | Augmented expander cycle |
RU2484286C1 (ru) * | 2011-12-07 | 2013-06-10 | Николай Борисович Болотин | Кислородно-водородный жидкостный ракетный двигатель |
FR2984452B1 (fr) * | 2011-12-14 | 2014-06-13 | Snecma | Dispositif et procede de pressurisation |
RU2484285C1 (ru) * | 2011-12-29 | 2013-06-10 | Николай Борисович Болотин | Кислородно-водородный жидкостный ракетный двигатель |
RU2551712C1 (ru) * | 2014-03-25 | 2015-05-27 | Открытое акционерное общество "Конструкторское бюро химавтоматики" | Жидкостный ракетный двигатель |
CN109578134B (zh) * | 2018-11-23 | 2020-10-23 | 北京宇航系统工程研究所 | 一种氢氧回收利用系统及其应用 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3077073A (en) * | 1957-10-29 | 1963-02-12 | United Aircraft Corp | Rocket engine having fuel driven propellant pumps |
US3049870A (en) * | 1960-04-14 | 1962-08-21 | United Aircraft Corp | Rocket propellant cycle |
DE1195092B (de) * | 1960-12-07 | 1965-06-16 | United Aircraft Corp | Vorrichtung zum Regeln der Treibmittelzufuhr in einer Fluessigkeitsrakete |
DE1626049A1 (de) * | 1967-01-21 | 1970-08-27 | Messerschmitt Boelkow Blohm | Fluessigkeitsraketentriebwerk in Hauptstrombauart |
DE1626082B1 (de) * | 1967-07-26 | 1970-06-25 | Erno Raumfahrttechnik Gmbh | Raketentriebwerk fuer fluessige treibstoffe |
DE2743983C2 (de) * | 1977-09-30 | 1982-11-11 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Flüssigkeitsraketentriebwerk in Nebenstrombauart für den Betrieb im luftleeren Raum |
DE3328117A1 (de) * | 1983-08-04 | 1985-02-14 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Verfahren zum betreiben eines nebenstrom-raketentriebwerkes |
-
1985
- 1985-02-27 DE DE19853506826 patent/DE3506826A1/de active Granted
-
1986
- 1986-02-13 FR FR8601984A patent/FR2577996B1/fr not_active Expired - Lifetime
- 1986-02-27 JP JP4050786A patent/JPS61201871A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
JPS61201871A (ja) | 1986-09-06 |
DE3506826C2 (ru) | 1989-03-23 |
FR2577996A1 (fr) | 1986-08-29 |
DE3506826A1 (de) | 1986-08-28 |
FR2577996B1 (fr) | 1991-04-05 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4879874A (en) | Liquid fuel rocket engine | |
JPH0452859B2 (ru) | ||
US5417053A (en) | Partial regenerative dual fluid cycle gas turbine assembly | |
US5099645A (en) | Liquid-solid propulsion system and method | |
US3077073A (en) | Rocket engine having fuel driven propellant pumps | |
US4998410A (en) | Hybrid staged combustion-expander topping cycle engine | |
US3525223A (en) | Thermodynamic rocket process using alkali metal fuels in a two phase flow | |
US8572948B1 (en) | Rocket engine propulsion system | |
RU2641791C2 (ru) | Способ и устройство для питания ракетного двигателя | |
JPH0235843B2 (ru) | ||
US5233823A (en) | High-efficiency gas turbine engine | |
RU2155273C1 (ru) | Жидкостный ракетный двигатель (жрд) на криогенном топливе с замкнутым контуром привода турбины турбонасосного агрегата (варианты) | |
US5267437A (en) | Dual mode rocket engine | |
US4223530A (en) | Liquid fuel rocket engine having a propellant component pump turbine with a secondary thrust discharge and to a method of operating a liquid fuel rocket engine | |
US20020088221A1 (en) | Method and device for generating hot combustion waste gases | |
JPH0341668B2 (ru) | ||
US5135184A (en) | Propellant utilization system | |
US7926276B1 (en) | Closed cycle Brayton propulsion system with direct heat transfer | |
US3334486A (en) | Continuous flow combustion engine | |
RU2095607C1 (ru) | Жидкостный ракетный двигатель на криогенном топливе | |
RU2065985C1 (ru) | Трехкомпонентный жидкостный ракетный двигатель | |
JP2680288B2 (ja) | 蒸気噴射ガスタービンシステムおよびその運転方法 | |
US3984784A (en) | Expander open cycle gas dynamic laser | |
RU2187684C2 (ru) | Способ работы жидкостного ракетного двигателя и жидкостной ракетный двигатель | |
RU2233990C2 (ru) | Кислородно-керосиновый жидкостный ракетный двигатель с тепловым модулем, тепловой модуль и способ получения бессажевого газа в тепловом модуле |