FR2811018B1 - Materiau ablatif, destine a l'isolation ou la protection thermique d'un assemblage de moteur de fusee, comprenant un renforcement polyamide - Google Patents

Materiau ablatif, destine a l'isolation ou la protection thermique d'un assemblage de moteur de fusee, comprenant un renforcement polyamide

Info

Publication number
FR2811018B1
FR2811018B1 FR0108765A FR0108765A FR2811018B1 FR 2811018 B1 FR2811018 B1 FR 2811018B1 FR 0108765 A FR0108765 A FR 0108765A FR 0108765 A FR0108765 A FR 0108765A FR 2811018 B1 FR2811018 B1 FR 2811018B1
Authority
FR
France
Prior art keywords
fusee
insulation
thermal protection
engine assembly
ablative material
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 - Fee Related
Application number
FR0108765A
Other languages
English (en)
Other versions
FR2811018A1 (fr
Inventor
Kenneth P Wilson
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.)
Northrop Grumman Innovation Systems LLC
Original Assignee
Alliant Techsystems Inc
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 Alliant Techsystems Inc filed Critical Alliant Techsystems Inc
Publication of FR2811018A1 publication Critical patent/FR2811018A1/fr
Application granted granted Critical
Publication of FR2811018B1 publication Critical patent/FR2811018B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K9/97—Rocket nozzles
    • F02K9/974—Nozzle- linings; Ablative coatings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/403—Solid propellant rocket engines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/52—Protection, safety or emergency devices; Survival aids
    • B64G1/58—Thermal protection, e.g. heat shields
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/40—Organic materials
    • F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
    • F05D2300/433—Polyamides, e.g. NYLON
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/40—Organic materials
    • F05D2300/44—Resins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/614—Fibres or filaments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/70—Treatment or modification of materials
    • F05D2300/702—Reinforcement
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1028—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49346—Rocket or jet device making

Landscapes

  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Thermal Sciences (AREA)
  • Critical Care (AREA)
  • Health & Medical Sciences (AREA)
  • Emergency Medicine (AREA)
  • General Health & Medical Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Artificial Filaments (AREA)
  • Reinforced Plastic Materials (AREA)
  • Nonwoven Fabrics (AREA)
  • Inorganic Fibers (AREA)
FR0108765A 2000-06-30 2001-07-02 Materiau ablatif, destine a l'isolation ou la protection thermique d'un assemblage de moteur de fusee, comprenant un renforcement polyamide Expired - Fee Related FR2811018B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US21506400P 2000-06-30 2000-06-30

Publications (2)

Publication Number Publication Date
FR2811018A1 FR2811018A1 (fr) 2002-01-04
FR2811018B1 true FR2811018B1 (fr) 2006-06-02

Family

ID=22801485

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0108765A Expired - Fee Related FR2811018B1 (fr) 2000-06-30 2001-07-02 Materiau ablatif, destine a l'isolation ou la protection thermique d'un assemblage de moteur de fusee, comprenant un renforcement polyamide

Country Status (3)

Country Link
US (1) US20030200656A1 (fr)
JP (1) JP2002180904A (fr)
FR (1) FR2811018B1 (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
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US7093337B1 (en) * 2000-05-25 2006-08-22 Taylor Zachary R Integrated tankage for propulsion vehicles and the like
US8256086B2 (en) * 2009-06-25 2012-09-04 Lockheed Martin Corporation Method of producing missile nose cones
US20110024165A1 (en) 2009-07-31 2011-02-03 Raytheon Company Systems and methods for composite structures with embedded interconnects
US8826640B2 (en) * 2010-11-12 2014-09-09 Raytheon Company Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof
US20130337246A1 (en) * 2012-06-15 2013-12-19 3M Innovative Properties Company Electrical insulation material
JP6373057B2 (ja) * 2014-05-15 2018-08-15 株式会社Ｉｈｉエアロスペース 固体ロケットモータとその製造方法
CN105416564A (zh) * 2015-12-13 2016-03-23 张彬 一种高速飞行器破障装置
CN109989852B (zh) * 2019-03-29 2020-05-12 湖北航天技术研究院总体设计所 一种装药燃烧室壳体及其成型方法
CN113775437B (zh) * 2021-11-11 2022-02-15 北京玻钢院复合材料有限公司 一种复合材料固体火箭发动机绝热结构及成型方法
CN114964799B (zh) * 2022-04-28 2023-09-29 南京航空航天大学 火箭发动机扩张段多温度梯度下的状态监测系统及方法
KR102744281B1 (ko) * 2022-05-13 2024-12-17 한화에어로스페이스 주식회사 열경화성 페놀수지 조성물, 상기 조성물 함침 프리프레그, 및 상기 프리프레그를 포함하는 로켓 노즐 제조용 복합재료
CN115450798B (zh) * 2022-10-31 2024-10-11 北京中科宇航技术有限公司 长时间工作的固体火箭发动机及其长尾喷管

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3314915A (en) * 1962-11-02 1967-04-18 Taylor Corp Molding composition for making thermal barriers and method of making same
US3635675A (en) * 1968-05-28 1972-01-18 Us Air Force Preparation of graphite yarns
US3573086A (en) * 1968-12-10 1971-03-30 Atomic Energy Commission Fibrous carbon or graphite products and method of making same
US4381639A (en) * 1980-06-19 1983-05-03 Record Industrial Company Sheath-core yarn for severe thermal protecting fabrics and method therefor
GB2191115B (en) * 1980-12-18 1988-05-11 Secr Defence Ablative material
US4492779A (en) * 1981-12-07 1985-01-08 Thiokol Corporation Aramid polymer and powder filler reinforced elastomeric composition for use as a rocket motor insulation
JPS6197477A (ja) * 1984-10-19 1986-05-15 東邦レーヨン株式会社 炭素繊維製造用原糸
US4878431A (en) * 1986-02-21 1989-11-07 Hercules Incorporated Elastomeric insulating materials for rocket motors
JPH0233457A (ja) * 1988-07-22 1990-02-02 Nissan Motor Co Ltd ロケットモータケース用インシュレーション材
JP2506448B2 (ja) * 1989-06-16 1996-06-12 日産自動車株式会社 ロケットモ―タケ―ス用インシュレ―ション材
US5762746A (en) * 1989-08-16 1998-06-09 Thiokol Corporation Method of internally insulating a propellant combustion chamber
US5298313A (en) * 1990-01-31 1994-03-29 Ketema Inc. Ablative and insulative structures and microcellular carbon fibers forming same
FR2665860B1 (fr) * 1990-08-14 1994-04-08 Aerospatiale Ste Nationale Indle Dispositif de protection thermique de la paroi interne d'une structure creuse soumise a un ecoulement ablatif et son procede de fabrication.
US5498649A (en) * 1993-05-18 1996-03-12 Thiokol Corporation Low density thermoplastic elastomeric insulation for rocket motors
US5767221A (en) * 1995-05-24 1998-06-16 Thiokol Corporation Robust propellant liner and interfacial propellant burn rate control
US5821284A (en) * 1995-10-27 1998-10-13 The United States Of America As Represented By The Secretary Of The Air Force Durable motor insulation
US6479148B1 (en) * 1998-08-19 2002-11-12 Cordant Technologies Inc. Rocket assembly ablative materials formed from solvent-spun cellulosic precursors, and method of insulating or thermally protecting a rocket assembly with the same
JP2002523669A (ja) * 1998-08-19 2002-07-30 コーダント・テクノロジーズ・インコーポレーテッド ステープルセルロースファイバを先駆物質として形成されたロケットアッセンブリの削摩材、及びロケットアッセンブリをこれによって断熱する即ち熱的に保護する方法

Also Published As

Publication number Publication date
US20030200656A1 (en) 2003-10-30
JP2002180904A (ja) 2002-06-26
FR2811018A1 (fr) 2002-01-04

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ST Notification of lapse

Effective date: 20080331