ATE338204T1 - Methode zur herstellung eines isolierten raketengehäuses und entsprechendes raketenghäuse - Google Patents

Methode zur herstellung eines isolierten raketengehäuses und entsprechendes raketenghäuse

Info

Publication number
ATE338204T1
ATE338204T1 AT02009900T AT02009900T ATE338204T1 AT E338204 T1 ATE338204 T1 AT E338204T1 AT 02009900 T AT02009900 T AT 02009900T AT 02009900 T AT02009900 T AT 02009900T AT E338204 T1 ATE338204 T1 AT E338204T1
Authority
AT
Austria
Prior art keywords
rocket case
producing
insulated
strip
heat
Prior art date
Application number
AT02009900T
Other languages
English (en)
Inventor
Enrico Fazio
Paolo Bellomi
Original Assignee
Avio Spa
Agenzia Spaziale Italiana
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 Avio Spa, Agenzia Spaziale Italiana filed Critical Avio Spa
Application granted granted Critical
Publication of ATE338204T1 publication Critical patent/ATE338204T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56—Winding and joining, e.g. winding spirally
    • B29C53/58—Winding and joining, e.g. winding spirally helically
    • B29C53/60—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels
    • B29C53/602—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels for tubular articles having closed or nearly closed ends, e.g. vessels, tanks, containers
    • 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F02K9/346—Liners, e.g. inhibitors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/80—Component parts, details or accessories; Auxiliary operations
    • B29C53/8008—Component parts, details or accessories; Auxiliary operations specially adapted for winding and joining
    • B29C53/8016—Storing, feeding or applying winding materials, e.g. reels, thread guides, tensioners
    • B29C2053/8025—Storing, feeding or applying winding materials, e.g. reels, thread guides, tensioners tensioning

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
AT02009900T 2001-12-12 2002-05-02 Methode zur herstellung eines isolierten raketengehäuses und entsprechendes raketenghäuse ATE338204T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT2001TO001161A ITTO20011161A1 (it) 2001-12-12 2001-12-12 Metodo per la realizzazione di un involucro coibentato per un propulsore a razzo, ed involucro coibentato per un propulsore a razzo realizza

Publications (1)

Publication Number Publication Date
ATE338204T1 true ATE338204T1 (de) 2006-09-15

Family

ID=11459332

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02009900T ATE338204T1 (de) 2001-12-12 2002-05-02 Methode zur herstellung eines isolierten raketengehäuses und entsprechendes raketenghäuse

Country Status (4)

Country Link
EP (1) EP1319823B1 (de)
AT (1) ATE338204T1 (de)
DE (1) DE60214322T2 (de)
IT (1) ITTO20011161A1 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2354842C2 (ru) * 2007-05-30 2009-05-10 Открытое акционерное общество Научно-производственное объединение "Искра" Способ формирования теплозащитного покрытия днища корпуса ракетного двигателя на твердом топливе из композиционного материала
DE102008012924A1 (de) * 2008-03-06 2009-09-10 Egeplast Werner Strumann Gmbh & Co. Kg Verfahren zur Herstellung eines Bauteils aus Kunststoff sowie nach diesem Verfahren hergestelltes Kunststoffbauteil
RU2453720C1 (ru) * 2010-12-30 2012-06-20 Открытое акционерное общество Научно-производственное объединение "Искра" Способ изготовления теплозащитного покрытия
RU2459105C1 (ru) * 2011-03-29 2012-08-20 Открытое акционерное общество Научно-производственное объединение "Искра" Способ изготовления сферической заглушки с фланцем для сопла ракетного двигателя
RU2460899C1 (ru) * 2011-05-31 2012-09-10 Открытое акционерное общество Научно-производственное объединение "Искра" Способ изготовления сферической заглушки с фланцем для сопла ракетного двигателя
RU2460900C1 (ru) * 2011-06-29 2012-09-10 Открытое акционерное общество Научно-производственное объединение "Искра" Способ изготовления сферической заглушки с фланцем для сопла ракетного двигателя
CN104029828B (zh) * 2014-05-07 2015-06-10 北京空间飞行器总体设计部 一种探测器发动机隔热装置
DE102015112636A1 (de) * 2015-07-31 2017-02-02 Deutsches Zentrum für Luft- und Raumfahrt e.V. Mantel einer Festbrennstoffrakete, Verfahren zu dessen Herstellung, Festbrennstoffrakete und Vorrichtung
RU2614422C2 (ru) * 2015-08-31 2017-03-28 Публичное акционерное общество Научно-производственное объединение "Искра" Способ изготовления корпуса ракетного двигателя твердого топлива
CN105292522B (zh) * 2015-11-09 2018-06-22 上海卫星装备研究所 航天器高温隔热屏安装装置及方法
RU2639417C1 (ru) * 2015-12-14 2017-12-21 Акционерное общество "Пермский завод "Машиностроитель" Способ нанесения теплозащитного покрытия на наружную поверхность корпусных изделий
ES2954896T3 (es) 2017-11-27 2023-11-27 Avio Spa Proceso de fabricación para la creación de un elemento de cúpula proporcionado con protección térmica para un motor cohete de propulsante sólido
RU2722994C1 (ru) * 2019-05-29 2020-06-05 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Ракетный двигатель на твёрдом топливе
EP4065634A4 (de) * 2019-11-26 2023-02-01 Government of The United States as Represented by the Secretary of the Air Force Faserverstärkte polymerverbundstrukturen und elektromagnetisches induktionsverfahren zu ihrer herstellung
FR3127434B1 (fr) * 2021-09-30 2023-11-10 Faurecia Systemes Dechappement Procédé de fabrication par enroulement
CN115288877B (zh) * 2022-08-11 2024-07-19 陕西星际荣耀空间科技有限责任公司 一种喷管扩张段一体性加强结构及其施工方法、喷管
CN115816879B (zh) * 2022-12-26 2026-02-10 山东非金属材料研究所 一种单封头发动机复合材料壳体制备方法
CN116220946B (zh) * 2023-02-22 2026-02-17 陕西凌空科技有限公司 一种固体火箭发动机的复合材料壳体及其成型方法
CN115898695B (zh) * 2023-03-09 2023-05-16 陕西普利美材料科技有限公司 一种固体火箭发动机燃烧室绝热层结构及其粘接方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2479828A (en) * 1947-11-20 1949-08-23 Aerojet Engineering Corp Propellant charge for rocket motors
FR1282930A (fr) * 1960-03-04 1962-01-27 Atlantic Res Corp Nouvelle charge propulsive solide à surface inhibée
US4596619A (en) * 1982-05-17 1986-06-24 Hercules Incorporated Process for lining composite vessels
FR2569237B1 (fr) * 1984-08-14 1987-01-09 Aerospatiale Dispositif de protection thermique resistant a l'ablation et aux vibrations, et un procede de fabrication
FR2614651B1 (fr) * 1987-04-28 1992-05-07 Europ Propulsion Procede et installation pour la formation d'un revetement de protection thermique d'un propulseur
US4909880A (en) * 1988-05-17 1990-03-20 General Dynamics Corporation Method and apparatus for tape winding on irregular shapes
US5145543A (en) * 1989-04-14 1992-09-08 Thiokol Corporation Combination filament winding and tape laying apparatus and method for making and using the same
FR2650217B1 (fr) * 1989-07-25 1991-10-25 Aerospatiale Procede et dispositif de revetement de protection thermique interne de propulseur
US5174845A (en) * 1990-05-14 1992-12-29 Thiokol Corporation Insulation wrapping strip with variable configuration

Also Published As

Publication number Publication date
ITTO20011161A1 (it) 2003-06-12
DE60214322T2 (de) 2007-09-13
EP1319823A2 (de) 2003-06-18
DE60214322D1 (de) 2006-10-12
EP1319823A3 (de) 2003-08-13
EP1319823B1 (de) 2006-08-30
ITTO20011161A0 (it) 2001-12-12

Similar Documents

Publication Publication Date Title
ATE338204T1 (de) Methode zur herstellung eines isolierten raketengehäuses und entsprechendes raketenghäuse
DE69632981D1 (de) Verschleisszusammensetzung, verfahren zur Herstellung einer Verschleisszusammensetzung und gasturbine Motor mit Verschleissdichtung
SE9201271D0 (sv) Flexible cord winding and packaging configuration and method of making such package
ATE421060T1 (de) Verbundstoffrohranordnung und dazugehöriges herstellungsverfahren
DE60121779D1 (de) Hochdruck verbundrohr und verfahren zur herstellung des rohres
DE69423061D1 (de) Gasturbinenschaufel, Verfahren zur Herstellung derselben sowie Gasturbine mit dieser Schaufel
DE3583810D1 (de) Verfahren zur herstellung eines mehrschichtigen rohres.
DE59605799D1 (de) Verstellbares planendach
DE60130372D1 (de) Tauchformen, zusammensetzung für das tauchformen und verfahren zur herstellung von tauchformen
ATE310195T1 (de) Mehrlagiger schlauch aus profiliertem bandmaterial
BR9606556A (pt) Processo e dispositivo para enrolamento continuo de uma folha em movímento
GB0029953D0 (en) Current sensor
ATE232161T1 (de) Kühlmittelrohr für brennkraftmaschinen sowie verfahren zur herstellung desselben
SE0003197L (sv) Magnetisk komponent med luftgap
ATE219209T1 (de) Schalldämpfereinsatz und verfahren zu dessen herstellung
BR8807791A (pt) Construcao de reforco de talao
FI962187A0 (fi) Menetelmä putkiyhteen valmistamiseksi ja putkiyhdeMenetelmä putkiyhteen valmistamiseksi ja putkiyhde
DE69712966D1 (de) Herstellungsverfahren für nahtlosen metallischen Gurt
SE8206092L (sv) Sett att tillverka filamentlindade foremal
DE69132390D1 (de) Verfahren zur herstellung eines elektromagnetischen wandlers
ATE175455T1 (de) Verfahren zur herstellung einer stopfbüchsenpackung
ES2124392T3 (es) Pieza conformada particularmente para uso como material de embalaje, metodo y aparato para su fabricacion y empleo.
DE59701267D1 (de) Abgasreinigungsvorrichtung für einen verbrennungsmotor sowie verfahren zu ihrer herstellung
ES2161300T3 (es) Perlas.
EP1229619A3 (de) Zündspule mit Abwicklungsschutz der Zündspulenprimärwicklung

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties