ITMI20021189A0 - Propulsore a razzo con separazione tra mantello interno e mantello esterno - Google Patents

Propulsore a razzo con separazione tra mantello interno e mantello esterno

Info

Publication number
ITMI20021189A0
ITMI20021189A0 IT2002MI001189A ITMI20021189A ITMI20021189A0 IT MI20021189 A0 ITMI20021189 A0 IT MI20021189A0 IT 2002MI001189 A IT2002MI001189 A IT 2002MI001189A IT MI20021189 A ITMI20021189 A IT MI20021189A IT MI20021189 A0 ITMI20021189 A0 IT MI20021189A0
Authority
IT
Italy
Prior art keywords
separation
internal
outer cloth
rocket thrusters
thrusters
Prior art date
Application number
IT2002MI001189A
Other languages
English (en)
Inventor
Herbert Linner
Original Assignee
Astrium Gmbh
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 Astrium Gmbh filed Critical Astrium Gmbh
Publication of ITMI20021189A0 publication Critical patent/ITMI20021189A0/it
Publication of ITMI20021189A1 publication Critical patent/ITMI20021189A1/it

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
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • 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
    • F02K9/97—Rocket nozzles
    • F02K9/972—Fluid cooling arrangements for nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Toys (AREA)
IT2002MI001189A 2001-06-01 2002-05-31 Propulsore a razzo con separazione tra mantello interno e mantello esterno ITMI20021189A1 (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE10126923A DE10126923B4 (de) 2001-06-01 2001-06-01 Raketentriebwerk mit Trennung von Innenmantel und Außenmantel

Publications (2)

Publication Number Publication Date
ITMI20021189A0 true ITMI20021189A0 (it) 2002-05-31
ITMI20021189A1 ITMI20021189A1 (it) 2003-12-01

Family

ID=7687019

Family Applications (1)

Application Number Title Priority Date Filing Date
IT2002MI001189A ITMI20021189A1 (it) 2001-06-01 2002-05-31 Propulsore a razzo con separazione tra mantello interno e mantello esterno

Country Status (5)

Country Link
US (1) US6668543B2 (it)
JP (1) JP4057844B2 (it)
DE (1) DE10126923B4 (it)
FR (1) FR2825416B1 (it)
IT (1) ITMI20021189A1 (it)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008011502A1 (de) * 2008-02-25 2009-09-03 Deutsches Zentrum für Luft- und Raumfahrt e.V. Düsenerweiterung und Verfahren zur Herstellung einer Düsenerweiterung
US20100326045A1 (en) * 2009-02-13 2010-12-30 Blue Origin, Llc Multiple-use rocket engines and associated systems and methods
WO2010099228A1 (en) * 2009-02-24 2010-09-02 Blue Origin, Llc Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods
FR2963063B1 (fr) * 2010-07-26 2015-11-27 Snecma Chambre de combustion munie d'un element tubulaire
US9217389B1 (en) 2011-11-10 2015-12-22 Blue Origin, Llc Rocket turbopump valves and associated systems and methods
WO2015111253A1 (ja) * 2014-01-22 2015-07-30 株式会社Ihi スラスタ
FR3042542B1 (fr) * 2015-10-20 2017-12-01 Snecma Chambre propulsive et procede de fabrication
CN106438109A (zh) * 2016-10-31 2017-02-22 北京航天动力研究所 一种带喉部加强衬套的液体火箭发动机推力室夹层结构
CN108825406A (zh) * 2018-08-29 2018-11-16 北京航天动力研究所 一种液体火箭发动机推力室身部外壁结构
US11174966B1 (en) 2020-03-09 2021-11-16 Blue Origin, Llc Fluid damped check valve, and associated systems and mei'hods
US11391243B1 (en) 2020-03-09 2022-07-19 Blue Origin, Llc Seal for gimbaling and/or fixed rocket engine nozzles, and associated systems and methods
CN113153574B (zh) * 2021-04-22 2022-07-05 北京航天动力研究所 一种可重复使用的快捷连接夹层式燃烧室
CN113653571B (zh) * 2021-08-16 2022-11-08 北京机械设备研究所 固体推进剂的燃烧稳流装置及固体发动机燃烧发生器

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2395403A (en) * 1939-03-06 1946-02-26 Daniel And Florence Guggenheim Rotatable combustion apparatus for aircraft
US2520751A (en) * 1944-02-19 1950-08-29 Aerojet Engineering Corp Reaction motor with fluid cooling means
US2555081A (en) * 1946-03-26 1951-05-29 Daniel And Florence Guggenheim Means for supplying liquids to an annular rotating combustion chamber
US2706382A (en) * 1949-07-09 1955-04-19 Carborundum Co Devices for confinement and release of high velocity, hot gases
US2956399A (en) * 1956-11-16 1960-10-18 Clair M Beighley Fluid cooled homogeneous ceramic rocket motor wall structure
US2933888A (en) * 1956-11-23 1960-04-26 Africano Alfred Cooling system for a rocket engine
US3224193A (en) * 1963-06-25 1965-12-21 Curtiss Wright Corp Anisotropic heat shield construction
GB1148431A (en) * 1965-09-10 1969-04-10 Secr Defence Improvements in or relating to rocket projectiles
US4108241A (en) * 1975-03-19 1978-08-22 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Heat exchanger and method of making
US5701670A (en) * 1994-06-23 1997-12-30 Boeing North American, Inc. Method of making rocket engine combustion chamber utilizing "slide in" port liner
FR2733581B1 (fr) * 1995-04-27 1997-07-18 Europ Propulsion Enceinte de combustion avec refroidissement par transpiration
DE19602731C1 (de) * 1996-01-26 1997-07-10 Daimler Benz Aerospace Ag Wandstruktur für treibstoffgekühlte Triebwerkswände
DE19901422C2 (de) 1999-01-18 2000-11-16 Daimler Chrysler Ag Brennkammer-Kühlstruktur für ein Raketentriebwerk

Also Published As

Publication number Publication date
JP4057844B2 (ja) 2008-03-05
US20020178712A1 (en) 2002-12-05
FR2825416B1 (fr) 2006-12-01
DE10126923A1 (de) 2002-12-12
DE10126923B4 (de) 2006-11-23
FR2825416A1 (fr) 2002-12-06
US6668543B2 (en) 2003-12-30
ITMI20021189A1 (it) 2003-12-01
JP2003003907A (ja) 2003-01-08

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