DE3228162C2 - - Google Patents

Info

Publication number
DE3228162C2
DE3228162C2 DE19823228162 DE3228162A DE3228162C2 DE 3228162 C2 DE3228162 C2 DE 3228162C2 DE 19823228162 DE19823228162 DE 19823228162 DE 3228162 A DE3228162 A DE 3228162A DE 3228162 C2 DE3228162 C2 DE 3228162C2
Authority
DE
Germany
Prior art keywords
turbine
vacuum
fuel
hydrogen
combustion chamber
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
Application number
DE19823228162
Other languages
German (de)
English (en)
Other versions
DE3228162A1 (de
Inventor
Guenther Dr.-Ing. 8028 Taufkirchen De Schmidt
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Priority to DE19823228162 priority Critical patent/DE3228162A1/de
Priority to FR8312095A priority patent/FR2531141B1/fr
Priority to JP13690983A priority patent/JPS5941645A/ja
Publication of DE3228162A1 publication Critical patent/DE3228162A1/de
Application granted granted Critical
Publication of DE3228162C2 publication Critical patent/DE3228162C2/de
Granted legal-status Critical Current

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
    • F02K9/46—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)
  • Telescopes (AREA)
  • Jet Pumps And Other Pumps (AREA)
DE19823228162 1982-07-28 1982-07-28 Fluessigkeitsraketentriebwerk in nebenstrombauart fuer den betrieb im luftleeren raum Granted DE3228162A1 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE19823228162 DE3228162A1 (de) 1982-07-28 1982-07-28 Fluessigkeitsraketentriebwerk in nebenstrombauart fuer den betrieb im luftleeren raum
FR8312095A FR2531141B1 (fr) 1982-07-28 1983-07-21 Moteur-fusee a propergol liquide du type a courant derive pour le fonctionnement dans l'espace vide d'air
JP13690983A JPS5941645A (ja) 1982-07-28 1983-07-28 空気のない空間で駆動するための副流構造様式の液体ロケツト推進装置

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19823228162 DE3228162A1 (de) 1982-07-28 1982-07-28 Fluessigkeitsraketentriebwerk in nebenstrombauart fuer den betrieb im luftleeren raum

Publications (2)

Publication Number Publication Date
DE3228162A1 DE3228162A1 (de) 1984-02-09
DE3228162C2 true DE3228162C2 (US06312121-20011106-C00033.png) 1987-06-19

Family

ID=6169517

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19823228162 Granted DE3228162A1 (de) 1982-07-28 1982-07-28 Fluessigkeitsraketentriebwerk in nebenstrombauart fuer den betrieb im luftleeren raum

Country Status (3)

Country Link
JP (1) JPS5941645A (US06312121-20011106-C00033.png)
DE (1) DE3228162A1 (US06312121-20011106-C00033.png)
FR (1) FR2531141B1 (US06312121-20011106-C00033.png)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8610849D0 (en) * 1986-05-02 1986-08-20 Marconi Co Ltd Gas thruster
JPS62261652A (ja) * 1986-05-07 1987-11-13 Natl Space Dev Agency Japan<Nasda> 液体ロケツトエンジン
US4771600A (en) * 1986-10-20 1988-09-20 United Technologies Corporation Tripropellant rocket engine
US5267437A (en) * 1991-05-23 1993-12-07 United Technologies Corporation Dual mode rocket engine
RU2450153C1 (ru) * 2011-02-07 2012-05-10 Александр Фролович Ефимочкин Жидкостный ракетный двигатель
FR2981127B1 (fr) * 2011-10-11 2013-11-29 Snecma Dispositif de propulsion a reaction et procede d'alimentation
FR3012848B1 (fr) * 2013-11-06 2015-11-27 Snecma Ensemble propulsif et procede d'alimentation en ergols
RU2554126C1 (ru) * 2013-12-18 2015-06-27 Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" Объединенная двигательная установка ракетного блока
RU2612512C1 (ru) * 2016-03-29 2017-03-09 Владислав Юрьевич Климов Жидкостный ракетный двигатель
CN111409877A (zh) * 2020-03-13 2020-07-14 上海空间推进研究所 飞行器舱口加注管路吸空分离装置
RU2760956C1 (ru) * 2020-11-10 2021-12-01 Акционерное общество "КБхиммаш им. А.М. Исаева" Жидкостный ракетный двигатель с электронасосной системой подачи
CN114136635B (zh) * 2021-12-06 2022-08-23 北京航空航天大学 一种大流量快速响应固液火箭发动机地面输送系统

Family Cites Families (5)

* Cited by examiner, † Cited by third party
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
US3267664A (en) * 1963-03-19 1966-08-23 North American Aviation Inc Method of and device for cooling
US4171615A (en) * 1966-04-21 1979-10-23 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Supercharged topping rocket propellant feed system
DE2743983C2 (de) * 1977-09-30 1982-11-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Flüssigkeitsraketentriebwerk in Nebenstrombauart für den Betrieb im luftleeren Raum
JPS6131296A (ja) * 1984-07-24 1986-02-13 京セラミタ株式会社 書類等の記録資料の保管設備

Also Published As

Publication number Publication date
JPS5941645A (ja) 1984-03-07
FR2531141B1 (fr) 1987-03-20
FR2531141A1 (fr) 1984-02-03
JPH0341668B2 (US06312121-20011106-C00033.png) 1991-06-24
DE3228162A1 (de) 1984-02-09

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Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee