DE2059683B1 - Treibstoffsystem,insbesondere fuer Raketentriebwerke - Google Patents

Treibstoffsystem,insbesondere fuer Raketentriebwerke

Info

Publication number
DE2059683B1
DE2059683B1 DE19702059683D DE2059683DA DE2059683B1 DE 2059683 B1 DE2059683 B1 DE 2059683B1 DE 19702059683 D DE19702059683 D DE 19702059683D DE 2059683D A DE2059683D A DE 2059683DA DE 2059683 B1 DE2059683 B1 DE 2059683B1
Authority
DE
Germany
Prior art keywords
fuel
catalyst
control
capillary body
pressure
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.)
Pending
Application number
DE19702059683D
Other languages
German (de)
English (en)
Inventor
Wolfgang Mueller
German Dipl-Ing Munding
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
Publication of DE2059683B1 publication Critical patent/DE2059683B1/de
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/56Control
    • F02K9/58Propellant feed valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details not otherwise provided for
    • F02K9/68Decomposition chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
DE19702059683D 1970-12-04 1970-12-04 Treibstoffsystem,insbesondere fuer Raketentriebwerke Pending DE2059683B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2059683 1970-12-04

Publications (1)

Publication Number Publication Date
DE2059683B1 true DE2059683B1 (de) 1972-05-25

Family

ID=5789974

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19702059683D Pending DE2059683B1 (de) 1970-12-04 1970-12-04 Treibstoffsystem,insbesondere fuer Raketentriebwerke

Country Status (5)

Country Link
US (1) US3724213A (https=)
DE (1) DE2059683B1 (https=)
FR (1) FR2116403B1 (https=)
GB (1) GB1369466A (https=)
IT (1) IT941917B (https=)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4005607C1 (https=) * 1990-02-22 1991-07-25 Erno Raumfahrttechnik Gmbh, 2800 Bremen, De
US5819526A (en) * 1996-02-23 1998-10-13 Trw Inc. Low power arcjet propellant feed system
KR100657960B1 (ko) * 2005-05-17 2006-12-14 삼성에스디아이 주식회사 연료 전지 시스템 및 이를 구비하는 모바일 통신기기
CN111237086A (zh) * 2020-03-23 2020-06-05 北京宇航推进科技有限公司 带电连接器自锁阀的安装固定装置
CN113357112A (zh) * 2021-07-02 2021-09-07 兰州空间技术物理研究所 一种推进剂供给模块及推力器起弧方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126701A (en) * 1964-03-31 Process for generating gases
US799856A (en) * 1904-10-21 1905-09-19 Charles Lemale Internal-combustion turbo-motor.
GB844528A (en) * 1957-01-30 1960-08-10 Bristol Siddeley Engines Ltd Improvements in or relating to ignition devices for propulsion engines of the continuous internal combustion type
US3062004A (en) * 1959-05-18 1962-11-06 United Aircraft Corp Rocket motor starter

Also Published As

Publication number Publication date
FR2116403A1 (https=) 1972-07-13
FR2116403B1 (https=) 1974-09-13
IT941917B (it) 1973-03-10
GB1369466A (en) 1974-10-09
US3724213A (en) 1973-04-03

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