JP2015202701A5 - - Google Patents

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Publication number
JP2015202701A5
JP2015202701A5 JP2014081352A JP2014081352A JP2015202701A5 JP 2015202701 A5 JP2015202701 A5 JP 2015202701A5 JP 2014081352 A JP2014081352 A JP 2014081352A JP 2014081352 A JP2014081352 A JP 2014081352A JP 2015202701 A5 JP2015202701 A5 JP 2015202701A5
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JP
Japan
Prior art keywords
ablator
resin
binder resin
material solution
fiber
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.)
Granted
Application number
JP2014081352A
Other languages
English (en)
Japanese (ja)
Other versions
JP6353686B2 (ja
JP2015202701A (ja
Filing date
Publication date
Application filed filed Critical
Priority to JP2014081352A priority Critical patent/JP6353686B2/ja
Priority claimed from JP2014081352A external-priority 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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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 true JP2015202701A5 (enExample) 2016-10-27
JP6353686B2 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 (enExample)
EP (1) EP3130544B1 (enExample)
JP (1) JP6353686B2 (enExample)
WO (1) WO2015156368A1 (enExample)

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
Publication number Priority date Publication date Assignee Title
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
US9522747B2 (en) * 2014-06-03 2016-12-20 Analytical Mechanics Associates, Inc. Inflatable deceleration apparatus
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

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