Low cost fabrication of HOPE-X all-composite prototype structure
Two strict requirements were to be adhered to in the development of HOPE-X: to shorten the manufacturing lead-time and to reduce the fabrication cost for the lightweight prototype structure of HOPE-X. To meet these requirements, the design team adopted an all-composite monocoque structure instead of...
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Veröffentlicht in: | Advanced composite materials 2005-01, Vol.14 (3), p.289-304 |
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creator | Uzawa, Kiyoshi Nishiwaki, Kozo Niitsu, Mayuki Kamita, Toru Kimura, Gaku |
description | Two strict requirements were to be adhered to in the development of HOPE-X: to shorten the manufacturing lead-time and to reduce the fabrication cost for the lightweight prototype structure of HOPE-X. To meet these requirements, the design team adopted an all-composite monocoque structure
instead of a conventional aluminum skin, stringer-frame structure. The all-composite structure was made of several large parts in order to reduce the total number of parts. These large parts were made by using the non-autoclave curing technique and assembled by bonding into a monocoque structure.
The high-accuracy large lay-up tool and the custom-made oven played important roles particularly during these manufacturing processes, leading to reduction in both lead-time and cost. The structural design and the manufacturing strategy for the prototype structure are described in this paper.
The development of the lay-up tool and the oven, which helped to realize low fabrication cost, is described here. |
doi_str_mv | 10.1163/1568551054922593 |
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instead of a conventional aluminum skin, stringer-frame structure. The all-composite structure was made of several large parts in order to reduce the total number of parts. These large parts were made by using the non-autoclave curing technique and assembled by bonding into a monocoque structure.
The high-accuracy large lay-up tool and the custom-made oven played important roles particularly during these manufacturing processes, leading to reduction in both lead-time and cost. The structural design and the manufacturing strategy for the prototype structure are described in this paper.
The development of the lay-up tool and the oven, which helped to realize low fabrication cost, is described here.</description><identifier>ISSN: 0924-3046</identifier><identifier>EISSN: 1568-5519</identifier><identifier>DOI: 10.1163/1568551054922593</identifier><language>eng</language><publisher>Taylor & Francis Group</publisher><subject>ALL-COMPOSITE STRUCTURE ; BONDED JOINT ; LARGE PARTS ; LOW COST ; NON-AUTOCLAVE CURING ; RE-ENTRY VEHICLE</subject><ispartof>Advanced composite materials, 2005-01, Vol.14 (3), p.289-304</ispartof><rights>Copyright Taylor & Francis Group, LLC 2005</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c499t-88e2fda32e032f85a5b6e7ea367f67fe3785a562851e5d8ba8aa532adfa87dfe3</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,777,781,27905,27906</link.rule.ids></links><search><creatorcontrib>Uzawa, Kiyoshi</creatorcontrib><creatorcontrib>Nishiwaki, Kozo</creatorcontrib><creatorcontrib>Niitsu, Mayuki</creatorcontrib><creatorcontrib>Kamita, Toru</creatorcontrib><creatorcontrib>Kimura, Gaku</creatorcontrib><title>Low cost fabrication of HOPE-X all-composite prototype structure</title><title>Advanced composite materials</title><description>Two strict requirements were to be adhered to in the development of HOPE-X: to shorten the manufacturing lead-time and to reduce the fabrication cost for the lightweight prototype structure of HOPE-X. To meet these requirements, the design team adopted an all-composite monocoque structure
instead of a conventional aluminum skin, stringer-frame structure. The all-composite structure was made of several large parts in order to reduce the total number of parts. These large parts were made by using the non-autoclave curing technique and assembled by bonding into a monocoque structure.
The high-accuracy large lay-up tool and the custom-made oven played important roles particularly during these manufacturing processes, leading to reduction in both lead-time and cost. The structural design and the manufacturing strategy for the prototype structure are described in this paper.
The development of the lay-up tool and the oven, which helped to realize low fabrication cost, is described here.</description><subject>ALL-COMPOSITE STRUCTURE</subject><subject>BONDED JOINT</subject><subject>LARGE PARTS</subject><subject>LOW COST</subject><subject>NON-AUTOCLAVE CURING</subject><subject>RE-ENTRY VEHICLE</subject><issn>0924-3046</issn><issn>1568-5519</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2005</creationdate><recordtype>article</recordtype><recordid>eNqNkEtLAzEUhYMoWKt7l7NyN5rH5IUbpdQHFOpCwV24zSQwMjOpSYbaf--UuupChQsXzj3f5XAQuiT4mhDBbggXinOCeaUp5ZodoclOKkdNH6MJ1rQqGa7EKTpL6QNjQiXXE3S3CJvChpQLD6vYWMhN6Ivgi6fly7x8L6BtSxu6dUhNdsU6hhzydu2KlONg8xDdOTrx0CZ38bOn6O1h_jp7KhfLx-fZ_aK0lda5VMpRXwOjDjPqFQe-Ek46YEL6cRyTO01QxYnjtVqBAuCMQu1ByXq8T9HV_u-Y4XNwKZuuSda1LfQuDMlQpQWTFfuHUSpJhByNeG-0MaQUnTfr2HQQt4Zgs-vUHHY6Ird7pOl9iB1sQmxrk2Hbhugj9LZJhv1Ciz_pQ8jkr8y-AdAujnQ</recordid><startdate>20050101</startdate><enddate>20050101</enddate><creator>Uzawa, Kiyoshi</creator><creator>Nishiwaki, Kozo</creator><creator>Niitsu, Mayuki</creator><creator>Kamita, Toru</creator><creator>Kimura, Gaku</creator><general>Taylor & Francis Group</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7QF</scope><scope>7SR</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>FR3</scope><scope>JG9</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20050101</creationdate><title>Low cost fabrication of HOPE-X all-composite prototype structure</title><author>Uzawa, Kiyoshi ; Nishiwaki, Kozo ; Niitsu, Mayuki ; Kamita, Toru ; Kimura, Gaku</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c499t-88e2fda32e032f85a5b6e7ea367f67fe3785a562851e5d8ba8aa532adfa87dfe3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2005</creationdate><topic>ALL-COMPOSITE STRUCTURE</topic><topic>BONDED JOINT</topic><topic>LARGE PARTS</topic><topic>LOW COST</topic><topic>NON-AUTOCLAVE CURING</topic><topic>RE-ENTRY VEHICLE</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Uzawa, Kiyoshi</creatorcontrib><creatorcontrib>Nishiwaki, Kozo</creatorcontrib><creatorcontrib>Niitsu, Mayuki</creatorcontrib><creatorcontrib>Kamita, Toru</creatorcontrib><creatorcontrib>Kimura, Gaku</creatorcontrib><collection>CrossRef</collection><collection>Aluminium Industry Abstracts</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Advanced composite materials</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Uzawa, Kiyoshi</au><au>Nishiwaki, Kozo</au><au>Niitsu, Mayuki</au><au>Kamita, Toru</au><au>Kimura, Gaku</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Low cost fabrication of HOPE-X all-composite prototype structure</atitle><jtitle>Advanced composite materials</jtitle><date>2005-01-01</date><risdate>2005</risdate><volume>14</volume><issue>3</issue><spage>289</spage><epage>304</epage><pages>289-304</pages><issn>0924-3046</issn><eissn>1568-5519</eissn><abstract>Two strict requirements were to be adhered to in the development of HOPE-X: to shorten the manufacturing lead-time and to reduce the fabrication cost for the lightweight prototype structure of HOPE-X. To meet these requirements, the design team adopted an all-composite monocoque structure
instead of a conventional aluminum skin, stringer-frame structure. The all-composite structure was made of several large parts in order to reduce the total number of parts. These large parts were made by using the non-autoclave curing technique and assembled by bonding into a monocoque structure.
The high-accuracy large lay-up tool and the custom-made oven played important roles particularly during these manufacturing processes, leading to reduction in both lead-time and cost. The structural design and the manufacturing strategy for the prototype structure are described in this paper.
The development of the lay-up tool and the oven, which helped to realize low fabrication cost, is described here.</abstract><pub>Taylor & Francis Group</pub><doi>10.1163/1568551054922593</doi><tpages>16</tpages></addata></record> |
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subjects | ALL-COMPOSITE STRUCTURE BONDED JOINT LARGE PARTS LOW COST NON-AUTOCLAVE CURING RE-ENTRY VEHICLE |
title | Low cost fabrication of HOPE-X all-composite prototype structure |
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