دورية أكاديمية
ACCURACY OF RE-ENTRY FLIGHT TEST DATA NEEDED TO DETERMINE RE-ENTRY AERO-THERMODYNAMIC PARAMETERS
| العنوان: | ACCURACY OF RE-ENTRY FLIGHT TEST DATA NEEDED TO DETERMINE RE-ENTRY AERO-THERMODYNAMIC PARAMETERS |
|---|---|
| المؤلفون: | Dore, F. J. |
| المساهمون: | GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA |
| المصدر: | DTIC AND NTIS |
| سنة النشر: | 1954 |
| المجموعة: | Defense Technical Information Center: DTIC Technical Reports database |
| مصطلحات موضوعية: | Surface-launched Guided Missiles, Thermodynamics, ATMOSPHERE ENTRY), THERMAL STRESSES), (*SURFACE TO SURFACE MISSILES, (*NOSE CONES, REENTRY VEHICLES, TELEMETERING DATA, ACCURACY, AERODYNAMIC HEATING, HEAT TRANSFER, LAMINAR BOUNDARY LAYER, ANGLE OF ATTACK, DRAG, SURFACE TEMPERATURE, MATHEMATICAL ANALYSIS, CONICAL BODIES, PRESSURE, TITAN |
| الوصف: | This memorandum establishes accuracy requirements for the various items measured during re-entry for the determination of nose cone aero-thermodynamic parameters. The results are applicable, unless otherwise specified, for a variety of nose cone configurations and re-entry trajectories typical of 7-1, 7-3 and 7-0 missiles. (Author) |
| نوع الوثيقة: | text |
| وصف الملف: | text/html |
| اللغة: | English |
| العلاقة: | http://www.dtic.mil/docs/citations/AD0831415Test |
| الإتاحة: | http://www.dtic.mil/docs/citations/AD0831415Test http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=AD0831415Test |
| حقوق: | APPROVED FOR PUBLIC RELEASE |
| رقم الانضمام: | edsbas.DF859A06 |
| قاعدة البيانات: | BASE |
| الوصف غير متاح. |