Academic Journal
Predicting the Initial Crack Length in a Solid Propellant
العنوان: | Predicting the Initial Crack Length in a Solid Propellant |
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المؤلفون: | Liu, C. T., Kwon, Y. G., Hendrickson, T. L. |
المساهمون: | AIR FORCE RESEARCH LAB EDWARDS AFB CA SPACE AND MISSILE PROPULSION DIV |
المصدر: | DTIC AND NTIS |
سنة النشر: | 2001 |
المجموعة: | Defense Technical Information Center: DTIC Technical Reports database |
مصطلحات موضوعية: | Solid Rocket Propellants, STRESS STRAIN RELATIONS, SOLID PROPELLANTS, CRACKS, MATHEMATICAL PREDICTION, CRACK LENGTHS, PRESENTATION SLIDES, VIEWGRAPHS ONLY, WUAFRL2303M1G2346120 |
الوصف: | Prepared in collaboration with Naval Postgraduate School and Thiokol Co. Presented at the JANNAF Structures and Mechanical Behavior Subcommittee Meeting (34th) held in Cocoa Beach, FL on 26-30 March 2001. |
نوع الوثيقة: | text |
وصف الملف: | text/html |
اللغة: | English |
Relation: | http://www.dtic.mil/docs/citations/ADA410508 |
الاتاحة: | http://www.dtic.mil/docs/citations/ADA410508 http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA410508 |
Rights: | APPROVED FOR PUBLIC RELEASE |
رقم الانضمام: | edsbas.464C922C |
قاعدة البيانات: | BASE |
الوصف غير متاح. |