Electronic Resource

Development of Advanced Interceptor Substructural Material.

التفاصيل البيبلوغرافية
العنوان: Development of Advanced Interceptor Substructural Material.
المؤلفون: GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV, Adsit,Norman R, Hertz,Julius
المصدر: DTIC AND NTIS
بيانات النشر: 1981-07
نوع الوثيقة: Electronic Resource
مستخلص: The work reported herein is aimed at the development of ultra-high-modulus graphite/epoxy structures for use in future advanced terminal interceptors (ATI). The work has shown that gore section layup used to fabricate interceptor frusta do not effect the strength or modulus of the frusta. Tests on flat panels representation of full thickness joints substantiated that the end joints will carry ATI loads. Finally, two short but full thickness frusta with antenna window cutouts were fabricated and tested. These frusta met the design goals. Analysis work has been completed and the design and materials are ready for a full-scale demonstration. To accomplish this, the preliminary design was reviewed and has been updated. A full-scale tool was designed and has been procured. Finally, a manufacturing process plan for the full-scale frustum was prepared.
مصطلحات الفهرس: Laminates and Composite Materials, Guided Missiles, COMPOSITE MATERIALS, FIBER REINFORCED COMPOSITES, COMPOSITE STRUCTURES, INTERCEPTORS, GUIDED MISSILES, MANUFACTURING, SCALE MODELS, EXPERIMENTAL DESIGN, STRUCTURAL ANALYSIS, TEST METHODS, FABRICATION, GRAPHITE, THERMAL ANALYSIS, SHEAR STRESSES, AIRFRAMES, TITANIUM, RINGS, EPOXY RESINS, FRUSTUMS, ANTENNA WINDOWS, JOINTS, PE62113A, AS661, Text
URL: https://apps.dtic.mil/docs/citations/ADA103836
الاتاحة: Open access content. Open access content
APPROVED FOR PUBLIC RELEASE
ملاحظة: text/html
English
Other Numbers: DTICE ADA103836
831807812
المصدر المساهم: From OAIster®, provided by the OCLC Cooperative.
رقم الانضمام: edsoai.ocn831807812
قاعدة البيانات: OAIster