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1دورية أكاديمية
المؤلفون: White, E. J.
المساهمون: GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Surface-launched Guided Missiles, Combustion and Ignition, Liquid Propellant Rocket Engines, IGNITION CIRCUITS, IGNITION, EXPLOSIVES INITIATORS, LIQUID PROPELLANT ROCKET ENGINES, SURFACE TO SURFACE MISSILES, STAGING, AUTOMATIC PILOTS, INSTRUCTION MANUALS, NOSE CONES, UMBILICAL CORDS(AEROSPACE), CHECKOUT EQUIPMENT, OPERATION, INSTALLATION, TEST METHODS, MAINTENANCE, REENTRY VEHICLES, ATLAS, XSM-65D MISSILES
وصف الملف: text/html
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2دورية أكاديمية
المؤلفون: Wray, K L, Rose, P H, Koritz, H E
المساهمون: AVCO EVERETT RESEARCH LAB INC EVERETT MA
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Reentry Vehicles, Unmanned Spacecraft, REENTRY VEHICLES, ABLATION, BOUNDARY LAYER, CONTAMINATION, HALOCARBON PLASTICS, HIGH TEMPERATURE, INFRARED SPECTRA, INTENSITY, MODEL TESTS, NITROGEN, NOSE CONES, PHOTOMULTIPLIER TUBES, SIMULATION, SPECTROPHOTOMETERS, SPECTROSCOPY, SPECTRUM ANALYZERS, TEST METHODS, THERMAL RADIATION, TURBULENT BOUNDARY LAYER, TWO DIMENSIONAL FLOW, ULTRAVIOLET SPECTRA, VISIBLE SPECTRA, DELRIN, TETRAFLUOROETHYLENE RESINS
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3دورية أكاديمية
المؤلفون: Demetriades, A
المساهمون: PHILCO-FORD CORP NEWPORT BEACH CA SPACE AND RE-ENTRY SYSTEMS DIV
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, WAKE, ANEMOMETERS, ANGLE OF ATTACK, ATMOSPHERE ENTRY, AXISYMMETRIC FLOW, BOUNDARY LAYER TRANSITION, DRAG, ELECTRON DENSITY, EXHAUST NOZZLES, HEAT TRANSFER, MATHEMATICAL ANALYSIS, NOSE CONES, PENETRATION, PLASMA JETS, REENTRY VEHICLES, SHOCK WAVES, SUPERSONIC CHARACTERISTICS, SUPERSONIC FLOW, TEMPERATURE, TEST EQUIPMENT, TEST METHODS, TURBULENCE, TURBULENT BOUNDARY LAYER, TWO DIMENSIONAL FLOW, VELOCITY, VISCOSITY, WIND TUNNEL MODELS, HOT-WIRE ANEMOMETERS
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4دورية أكاديمية
المؤلفون: WARREN, W. R., KAEGI, E. M., HARRIS, C. J., GEIGER, R. E.
المساهمون: GENERAL ELECTRIC CO PHILADELPHIA PA MISSILE AND SPACE DIV
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Test Facilities, Equipment and Methods, Spacecraft Trajectories and Reentry, SHOCK TUNNELS, NOSE CONES, SHOCK TUBES, ATMOSPHERE ENTRY, BOUNDARY LAYER, MODEL TESTS, PRESSURE, HYPERSONIC CHARACTERISTICS, LIFT, HYPERSONIC WIND TUNNELS, WIND TUNNEL MODELS, HYPERSONIC FLOW, RESISTANCE THERMOMETERS, TEST METHODS, SHOCK WAVES, PIEZOELECTRIC GAGES, HEAT TRANSFER, REENTRY VEHICLES
وصف الملف: text/html
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5دورية أكاديمية
المؤلفون: Lindberg, H. E., Firth, R. D.
المساهمون: STANFORD RESEARCH INST MENLO PARK CA POULTER LABS
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Test Facilities, Equipment and Methods, Fluid Mechanics, BLAST, SHOCK TUBES, REENTRY VEHICLES, SIMULATORS, SHOCK WAVES, EXPLOSIVE CHARGES, NOSE CONES, TEST METHODS, EXPLOSION EFFECTS, TIME, AERODYNAMIC LOADING
وصف الملف: text/html
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6دورية أكاديمية
المساهمون: KAMAN AIRCRAFT CORP BLOOMFIELD CONN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: ROTORCHUTES, RECOVERABLE BOOSTER ENGINES, ATMOSPHERE ENTRY, RECOVERY, DRAG, FLIGHT PATHS, DESCENT TRAJECTORIES, WEIGHT, STABILITY, DECELERATION, MODEL TESTS, WIND TUNNEL MODELS, TRANSONIC CHARACTERISTICS, TEST METHODS, CENTRIFUGAL FIELDS, PERFORMANCE(ENGINEERING), SPRINGS, LOAD DISTRIBUTION, FLIGHT TESTING, NOSE CONES, MANNED SPACECRAFT, LIFT, TORQUE, MOMENTS, CONTROL, CONTROL SYSTEMS, REENTRY VEHICLES, LANDING, FORCE
وصف الملف: text/html
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7دورية أكاديمية
المؤلفون: Spencer,D. J.
المساهمون: AEROSPACE CORP EL SEGUNDO CALIF
المصدر: DTIC AND NTIS
مصطلحات موضوعية: FLAME SPRAYING, NOSE CONES, REFRACTORY MATERIALS, TEST FACILITIES, ABLATION, AERODYNAMIC HEATING, ANALOG COMPUTERS, ATMOSPHERE ENTRY, CERAMIC COATINGS, ELECTRIC ARCS, ENTHALPY, GAS FLOW, HEAT TRANSFER, HEAT RESISTANT PLASTICS, HYPERSONIC FLOW, HYPERSONIC WIND TUNNELS, MATERIALS, MEASUREMENT, METAL COATINGS, PLASMA JETS, PLASTIC COATINGS, REENTRY VEHICLES, REFRACTORY COATINGS, SIMULATION, TEST EQUIPMENT, TEST METHODS, TUNGSTEN, TURBULENCE
وصف الملف: text/html
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8دورية أكاديمية
المؤلفون: Richards,Bryan E.
المساهمون: VON KARMAN INST FOR FLUID DYNAMICS RHODE-SAINT-GENESE (BELGIUM)
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Reentry Vehicles, Thermodynamics, Reentry vehicles, Hypersonic characteristics, Nose cones, Heat transfer, Reynolds number, Aerodynamic configurations, Hemispheres, Conical bodies, Surface roughness, Boundary layer transition, Test methods, Test equipment, Pressure measurement, Laminar boundary layer, Turbulent boundary layer
وصف الملف: text/html
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9دورية أكاديمية
المؤلفون: Bauer,R. C., Riddle,C. D.
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AIR FORCE STATION TENN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missiles, Reentry vehicles, Nose cones, Transonic characteristics, Wind tunnel tests, Dynamics, Stability, Afterbodies, Test equipment, Test methods, Model tests, Jupiter W14 reentry configuration
وصف الملف: text/html
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10دورية أكاديمية
المؤلفون: Softley,E. J., Muntz,E. P., Zempel,R. E.
المساهمون: GENERAL ELECTRIC CO PHILADELPHIA PA MISSILE AND SPACE DIV
المصدر: DTIC AND NTIS
مصطلحات موضوعية: (*WAKE, HYPERSONIC CHARACTERISTICS), (*SLENDER BODIES, WAKE), REENTRY VEHICLES, NOSE CONES, LAMINAR FLOW, CONICAL BODIES, ATMOSPHERE ENTRY, TEST METHODS, ELECTRON BEAMS, ELECTROLUMINESCENCE, HYPERSONIC FLOW, RAREFIED GAS DYNAMICS, DENSITY, NITROGEN, AIR, TEMPERATURE, PRESSURE, MEASUREMENT, REYNOLDS NUMBER, BOUNDARY LAYER, BASE FLOW
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