FR2516172B3 - - Google Patents

Info

Publication number
FR2516172B3
FR2516172B3 FR8218953A FR8218953A FR2516172B3 FR 2516172 B3 FR2516172 B3 FR 2516172B3 FR 8218953 A FR8218953 A FR 8218953A FR 8218953 A FR8218953 A FR 8218953A FR 2516172 B3 FR2516172 B3 FR 2516172B3
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
Application number
FR8218953A
Other languages
French (fr)
Other versions
FR2516172A1 (fr
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 FR2516172A1 publication Critical patent/FR2516172A1/fr
Application granted granted Critical
Publication of FR2516172B3 publication Critical patent/FR2516172B3/fr
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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/18—Composite ram-jet/rocket engines
    • 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/805—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control servo-mechanisms or control devices therefor
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S60/00—Power plants
    • Y10S60/917—Solid fuel ramjet using pulverized fuel

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Taps Or Cocks (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
FR8218953A 1981-11-12 1982-11-10 Dispositif de soupape pour la commande de fluides en ecoulement a haute temperature, notamment pour le dosage des debits de gaz riches en combustible dans des moteurs-fusees du type statoreacteur Granted FR2516172A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3144936A DE3144936C1 (de) 1981-11-12 1981-11-12 Ventileinrichtung zum Steuern stroemender Medien hoher Temperatur,insbesondere zum Dosieren der Mengen brennstoffreicher Gase bei Staustrahl-Raketentriebwerken

Publications (2)

Publication Number Publication Date
FR2516172A1 FR2516172A1 (fr) 1983-05-13
FR2516172B3 true FR2516172B3 (US07714131-20100511-C00024.png) 1984-11-30

Family

ID=6146222

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8218953A Granted FR2516172A1 (fr) 1981-11-12 1982-11-10 Dispositif de soupape pour la commande de fluides en ecoulement a haute temperature, notamment pour le dosage des debits de gaz riches en combustible dans des moteurs-fusees du type statoreacteur

Country Status (4)

Country Link
US (1) US4483139A (US07714131-20100511-C00024.png)
DE (1) DE3144936C1 (US07714131-20100511-C00024.png)
FR (1) FR2516172A1 (US07714131-20100511-C00024.png)
GB (1) GB2109511A (US07714131-20100511-C00024.png)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3502673A1 (de) * 1985-01-26 1986-07-31 Rheinmetall GmbH, 4000 Düsseldorf Luftatmender feststoff-staustrahlantrieb
US5817968A (en) * 1987-08-03 1998-10-06 The United States Of America As Represented By The Secretary Of The Air Force Gas generation with high pressure sensitivity exponent propellant
US5172547A (en) * 1991-04-30 1992-12-22 The United States Of America As Represented By The Secretary Of The Air Force Electronic valve control for gas generator outflow
NO180467C (no) * 1994-11-04 1997-04-23 Rc Subsea As Strupeventil
US7287725B2 (en) * 2005-04-25 2007-10-30 Raytheon Company Missile control system and method
US7856806B1 (en) * 2006-11-06 2010-12-28 Raytheon Company Propulsion system with canted multinozzle grid
DE102007010349B4 (de) * 2007-03-03 2009-07-09 Lfk-Lenkflugkörpersysteme Gmbh Ventilsteuereinheit für Staustrahlantrieb sowie Lenkflugkörper mit einer solchen Ventilsteuereinheit
US8225507B2 (en) 2008-02-28 2012-07-24 The Aerospace Corporation Stereolithographic rocket motor manufacturing method
US8601790B2 (en) * 2008-02-28 2013-12-10 The Aerospace Corporation Buried radial flow rapid prototyping rocket motors
US8707676B2 (en) * 2008-02-28 2014-04-29 The Aerospace Corporation Radial flow rapid prototyping rocket motors
US8117847B2 (en) 2008-03-07 2012-02-21 Raytheon Company Hybrid missile propulsion system with reconfigurable multinozzle grid
US9038368B2 (en) 2011-08-01 2015-05-26 The Aerospace Corporation Systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor
US9429104B2 (en) 2011-08-01 2016-08-30 The Aerospace Corporation Systems and methods for casting hybrid rocket motor fuel grains
US9127622B2 (en) * 2011-11-21 2015-09-08 United Technologies Corporation Reversible flow discharge orifice
CN105736181A (zh) * 2014-12-09 2016-07-06 上海新力动力设备研究所 固体火箭发动机燃气流量调节装置环形多孔扰流结构

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1311642A (en) * 1919-07-29 Check-valve
DE133326C (US07714131-20100511-C00024.png) *
US2452441A (en) * 1944-06-17 1948-10-26 Alco Valve Co Regulator valve having a capillary tube expansion passage
US2948112A (en) * 1953-12-14 1960-08-09 Kenneth W Smith Combined rocket and ram-jet engine
US2935084A (en) * 1955-05-02 1960-05-03 Garrett Corp Air pressure regulator
US3065597A (en) * 1959-09-28 1962-11-27 Gen Electric Reignitable solid rocket motor
US3712058A (en) * 1961-08-14 1973-01-23 Northrop Carolina Inc Solid propellant controlled rocket motors
FR1378866A (fr) * 1963-07-11 1964-11-20 Onera (Off Nat Aerospatiale) Perfectionnements apportés aux générateurs de gaz chauds, notamment aux moteursfusées, à ergols fluide et solide hypergoliques
US3691770A (en) * 1966-12-02 1972-09-19 Us Navy Thrust control means for a solid propellant rocket motor
FR2109035A5 (US07714131-20100511-C00024.png) * 1970-05-11 1972-05-26 Aquitaine Petrole
DE3005864A1 (de) * 1980-02-16 1981-09-03 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zum steuern der stroemungsquerschnitte von kanaelen, insbesondere von gasleitrohren eines raketen-staustrahltriebwerks
DE3006298C2 (de) * 1980-02-20 1983-08-18 Daimler-Benz Ag, 7000 Stuttgart Elektrohydraulische Schalteinrichtung

Also Published As

Publication number Publication date
FR2516172A1 (fr) 1983-05-13
DE3144936C1 (de) 1983-03-10
US4483139A (en) 1984-11-20
GB2109511A (en) 1983-06-02

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Legal Events

Date Code Title Description
ST Notification of lapse