JP6353686B2 - 再突入機の製造方法 - Google Patents

再突入機の製造方法 Download PDF

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Publication number
JP6353686B2
JP6353686B2 JP2014081352A JP2014081352A JP6353686B2 JP 6353686 B2 JP6353686 B2 JP 6353686B2 JP 2014081352 A JP2014081352 A JP 2014081352A JP 2014081352 A JP2014081352 A JP 2014081352A JP 6353686 B2 JP6353686 B2 JP 6353686B2
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JP
Japan
Prior art keywords
ablator
resin
mass
granular
material solution
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.)
Active
Application number
JP2014081352A
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English (en)
Japanese (ja)
Other versions
JP2015202701A5 (OSRAM
JP2015202701A (ja
Inventor
愛一郎 塚原
愛一郎 塚原
文人 武田
文人 武田
惇子 渡邉
惇子 渡邉
信輔 武田
信輔 武田
井出　勇
勇 井出
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.)
Lignyte Co Ltd
Mitsubishi Heavy Industries Ltd
Original Assignee
Lignyte Co Ltd
Mitsubishi Heavy Industries Ltd
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 Lignyte Co Ltd, Mitsubishi Heavy Industries Ltd filed Critical Lignyte Co Ltd
Priority to JP2014081352A priority Critical patent/JP6353686B2/ja
Priority to US15/302,292 priority patent/US10647452B2/en
Priority to PCT/JP2015/061153 priority patent/WO2015156368A1/ja
Priority to EP15776733.6A priority patent/EP3130544B1/en
Publication of JP2015202701A publication Critical patent/JP2015202701A/ja
Publication of JP2015202701A5 publication Critical patent/JP2015202701A5/ja
Application granted granted Critical
Publication of JP6353686B2 publication Critical patent/JP6353686B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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    • 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
    • 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
    • B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • 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
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • 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
    • B29C69/00—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore
    • B29C69/001—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore a shaping technique combined with cutting, e.g. in parts or slices combined with rearranging and joining the cut parts
    • 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
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
    • B29C70/021—Combinations of fibrous reinforcement and non-fibrous material
    • B29C70/025—Combinations of fibrous reinforcement and non-fibrous material with particular filler
    • 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
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • 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
    • B64G1/62—Systems for re-entry into the earth's atmosphere; Retarding or landing devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3097—Cosmonautical vehicles; Rockets

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Composite Materials (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Thermal Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Critical Care (AREA)
  • General Health & Medical Sciences (AREA)
  • Emergency Medicine (AREA)
  • Oral & Maxillofacial Surgery (AREA)
  • Reinforced Plastic Materials (AREA)
  • Moulding By Coating Moulds (AREA)
JP2014081352A 2014-04-10 2014-04-10 再突入機の製造方法 Active JP6353686B2 (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2014081352A JP6353686B2 (ja) 2014-04-10 2014-04-10 再突入機の製造方法
US15/302,292 US10647452B2 (en) 2014-04-10 2015-04-09 Ablator, re-entry vehicle and method of manufacturing them
PCT/JP2015/061153 WO2015156368A1 (ja) 2014-04-10 2015-04-09 アブレータ及び再突入機並びにそれらの製造方法
EP15776733.6A EP3130544B1 (en) 2014-04-10 2015-04-09 Ablator, reentry vehicle, and methods respectively for manufacturing said ablator and said reentry vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2014081352A JP6353686B2 (ja) 2014-04-10 2014-04-10 再突入機の製造方法

Publications (3)

Publication Number Publication Date
JP2015202701A JP2015202701A (ja) 2015-11-16
JP2015202701A5 JP2015202701A5 (OSRAM) 2016-10-27
JP6353686B2 true JP6353686B2 (ja) 2018-07-04

Family

ID=54287940

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014081352A Active JP6353686B2 (ja) 2014-04-10 2014-04-10 再突入機の製造方法

Country Status (4)

Country Link
US (1) US10647452B2 (OSRAM)
EP (1) EP3130544B1 (OSRAM)
JP (1) JP6353686B2 (OSRAM)
WO (1) WO2015156368A1 (OSRAM)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6353686B2 (ja) * 2014-04-10 2018-07-04 三菱重工業株式会社 再突入機の製造方法
CN109955501B (zh) * 2019-04-04 2021-06-11 北京卫星制造厂有限公司 返回式飞船大尺寸扇弧面防热结构成型工艺方法

Family Cites Families (30)

* Cited by examiner, † Cited by third party
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US3520027A (en) * 1968-07-11 1970-07-14 Dow Chemical Co Apparatus for the incorporation of filamentary material in resinous matrix
US3962491A (en) * 1972-10-11 1976-06-08 Aisin Chemical Company, Limited Process for producing resin-coated sand particles for use in shell moles
US4151800A (en) * 1977-04-15 1979-05-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thermal insulation protection means
US4255483A (en) * 1977-06-14 1981-03-10 Mcdonnell Douglas Corporation Fire barrier compositions and composites
US4364991A (en) * 1980-09-25 1982-12-21 Mcdonnell Douglas Corporation Fire resistant compositions and composites
FR2586080B1 (fr) * 1985-08-12 1987-11-27 Centre Nat Etd Spatiales Element de protection thermique pour un engin soumis a des echauffements importants
JP3565370B2 (ja) * 1995-03-31 2004-09-15 株式会社アイ・エイチ・アイ・エアロスペース アブレーション方法およびアブレータ構造
JPH09239847A (ja) * 1996-03-14 1997-09-16 Nissan Motor Co Ltd 低密度ｆｒｐアブレータ
JP3644612B2 (ja) 1996-05-28 2005-05-11 株式会社アイ・エイチ・アイ・エアロスペース アブレータ材料およびその製造方法
US6136418A (en) * 1999-03-01 2000-10-24 Rotary Rocket Company Rapidly removable thermal protection system for reusable launch vehicle
US6280667B1 (en) * 1999-04-19 2001-08-28 Andersen Corporation Process for making thermoplastic-biofiber composite materials and articles including a poly(vinylchloride) component
US6264144B1 (en) * 1999-08-03 2001-07-24 Lockheed Martin Corporation Material assembly for an inflatable aerodynamic braking device for spacecraft deceleration and the like
JP3559797B2 (ja) * 2000-03-07 2004-09-02 独立行政法人 宇宙航空研究開発機構 アブレータ
WO2003045460A1 (en) * 2001-11-27 2003-06-05 Takiron Co., Ltd. Implant material and process for producing the same
US20040096619A1 (en) * 2002-11-11 2004-05-20 The Boeing Company Flexible insulation blanket having a ceramic matrix composite outer layer
US7732512B2 (en) * 2003-02-13 2010-06-08 Orient Chemical Industries Co., Ltd. Laser light transmitting colored polyolefin resin compositions and process for laser welding
US7219859B2 (en) * 2005-04-01 2007-05-22 Spacehab, Incorporated Multipurpose modular spacecraft
US9040646B2 (en) * 2007-10-04 2015-05-26 W. L. Gore & Associates, Inc. Expandable TFE copolymers, methods of making, and porous, expanded articles thereof
JP5263737B2 (ja) * 2008-07-15 2013-08-14 独立行政法人国立高等専門学校機構 熱防御複合材の製造方法
US7931962B1 (en) * 2009-05-14 2011-04-26 Lockheed Martin Corporation Pyrolizing flexible ablator material
JP5878298B2 (ja) * 2011-03-02 2016-03-08 リグナイト株式会社 断熱材用組成物及び断熱材
US9592923B1 (en) * 2011-10-24 2017-03-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Flexible ablators
JP5727923B2 (ja) 2011-12-12 2015-06-03 川崎重工業株式会社 アブレータ
JP6253871B2 (ja) * 2012-01-17 2017-12-27 三菱重工業株式会社 断熱材及びそれを備えた宇宙機、並びに断熱材の製造方法
JP5590686B2 (ja) * 2012-07-25 2014-09-17 独立行政法人国立高等専門学校機構 熱防御複合材の製造方法
US9656769B2 (en) * 2013-05-01 2017-05-23 Mohammad A. Mazed Heat shield for a spacecraft
JP6353686B2 (ja) * 2014-04-10 2018-07-04 三菱重工業株式会社 再突入機の製造方法
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US9475261B2 (en) * 2014-08-18 2016-10-25 The Boeing Company Dual layer sandwich for thermal management
US9475593B2 (en) * 2014-08-18 2016-10-25 The Boeing Company Dual layer sandwich for thermal management

Also Published As

Publication number Publication date
US10647452B2 (en) 2020-05-12
WO2015156368A1 (ja) 2015-10-15
EP3130544B1 (en) 2022-06-01
EP3130544A1 (en) 2017-02-15
JP2015202701A (ja) 2015-11-16
EP3130544A4 (en) 2017-05-24
US20170029140A1 (en) 2017-02-02

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