دورية أكاديمية
THEORETICAL EFFECTS OF REENTRY AERODYNAMIC HEATING ON THE EXTERNAL SKIN STRUCTURE OF AMRAD EXPERIMENT NUMBER ONE
العنوان: | THEORETICAL EFFECTS OF REENTRY AERODYNAMIC HEATING ON THE EXTERNAL SKIN STRUCTURE OF AMRAD EXPERIMENT NUMBER ONE |
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المؤلفون: | Burleson, W G, Reynolds, R A |
المساهمون: | ARMY MISSILE COMMAND REDSTONE ARSENAL AL SYSTEMS RESEARCH DIRECTORATE |
المصدر: | DTIC AND NTIS |
سنة النشر: | 1965 |
المجموعة: | Defense Technical Information Center: DTIC Technical Reports database |
مصطلحات موضوعية: | Fluid Mechanics, AERODYNAMIC HEATING, REENTRY VEHICLES, ABLATION, AIRFRAMES, ALUMINUM, ANTIMISSILE DEFENSE SYSTEMS, ATMOSPHERE ENTRY, BASE FLOW, BLUNT BODIES, CONICAL BODIES, DRAG, EQUATIONS, GLASS, GRAPHICS, GUIDED MISSILE TRAJECTORIES, HEAT SHIELDS, HEAT TRANSFER, MATHEMATICAL ANALYSIS, NOSE CONES, PHENOLIC PLASTICS, RADAR, RECOVERY, SEPARATION, SURFACE TEMPERATURE, TABLES(DATA), THEORY, THERMAL INSULATION, THICKNESS, VOLUME |
الوصف: | Calculated reentry aerodynamic heating effects on the external skin of an ICBM reentry test vehicle having a relatively low weight-to-drag ratio are presented in this report. The vehicle is a blunt cone with the aft portion designed to fail just after maximum heating and the forward portion designed to survive to impact. The tape-wound, reinforced plastic heat shield is subjected to maximum reentry heating rates between 1,250,000 and 6,500,00 kcal/sq m hr. Resulting external and internal surface temperature histories are given. Effects of extreme trajectory, vehicle characteristics, and atmosphere variations on the aluminum substructure temperature histories are discussed. |
نوع الوثيقة: | text |
وصف الملف: | text/html |
اللغة: | English |
العلاقة: | http://www.dtic.mil/docs/citations/AD0465896Test |
الإتاحة: | http://www.dtic.mil/docs/citations/AD0465896Test http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=AD0465896Test |
حقوق: | Approved for public release; distribution is unlimited. |
رقم الانضمام: | edsbas.B70F608C |
قاعدة البيانات: | BASE |
الوصف غير متاح. |