Missing data, clade support and “reticulation”: the molecular systematics of Heliconius and related genera (Lepidoptera: Nymphalidae) re‐examined
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Andrew V.Z. Brower↗
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Results for “Re”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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The Virtual Astronomical Observatory: Re-engineering access to astronomical data
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R.J. Hanisch↗
Optically Controlled Electron Transfer in a Re I Complex
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Egmont J. Rohwer↗
Composite Thermal Protection Systems for Manned Re-Entry Vehicles
Composite thermal protection for manned reentry vehicle
HEAT SHIELD↗
PILOTED SIMULATION STUDIES OF RE-ENTRY GUIDANCE AND CONTROL AT PARABOLIC VELOCITIES
Piloted simulation studies of reentry guidance and control at parabolic velocities
VELOCITY↗
A WIND-TUNNEL INVESTIGATION aT SUBSONIC aND LOW SUPERSONIC SPEEDS oF a RE-ENTRY VEHICLE WITH RETRACTABLE WINGS
Wind tunnel tests of blunt reentry vehicle with retractable wings
WING↗
SUBSONIC AERODYNAMIC CHARACTERISTICS OF DISK RE-ENTRY CONFIGURATIONS WITH ELLIPTIC CROSS SECTIONS AND THICKNESS-DIAMETER RATIOS OF 0.225 AND 0.325
Aerodynamics of disk reentry configurations, for manned space flight, with elliptic cross sections and thickness diameter ratios of 0.225 and 0.325
REENTRY VEHICLE↗
CALCULATED RESULTS FOR THE TRANSIENT HEATING AND MELTING PROCESS OF GLASS SHIELDS WITH VARIOUS MATERIAL PROPERTIES AT THE STAGNATION POINT OF A RE-ENTERING ICBM
Calculated results for transient heating and melting of glass shield at stagnation point of reentering icbm
SHIELDING↗
FREE-FLIGHT MEASUREMENTS OF STATIC AND DYNAMIC STABILITY OF MODELS OF THE PROJECT MERCURY RE-ENTRY CAPSULE AT MACH NUMBERS 3 AND 9.5
Static & dynamic stability of mercury reentry capsule scale models at mach 3 & 9.5
REENTRY VEHICLE↗
THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92
Longitudinal aerodynamic characteristics of blunt, lifting reentry vehicle at mach 0.92
BLUNT BODY↗
ABLATING HEAT SHIELDS FOR LOW-ANGLE RE-ENTRY
Reports on the ablation of teflon and polyethylene heat shields for low-angle reentry
POLYETHYLENE↗
NEW RE-ENTRY SHAPES. H
Heat transfer and heating mechanisms in new reentry nose cone shapes
HEAT TRANSFER↗
NON-EQUILIBRIUM AND EQUILIBRIUM RADIATION AT SUPERSATELLITE RE-ENTRY VELOCITIES
Presentation of engineering estimates of radiation heating of vehicles reentering the earths atmosphere from lunar or interplanetary missions
SPACECRAFT REENTRY↗
APPLICATIONS FOR PLASTICS IN AEROSPACE RE-ENTRY VEHICLES
Application of plastics as ablative materials in the design of ballistic and manned superorbital lifting reentry vehicles
HEAT SHIELD↗
FLOW FIELD IN HYPERSONIC RE-ENTRY
Analysis of a sphere moving at a uniform hypersonic velocity in a free molecular flow
REENTRY EFFECT↗
HYPERSONIC FLOW PROBLEMS DURING RE-ENTRY INTO THE ATMOSPHERE
Hypersonic flow difficulties encountered during atmospheric reentry of spacecraft
HYPERSONIC FLOW↗
RADIATION AND ABLATION COOLING FOR MANNED RE-ENTRY VEHICLES
Comparison of foamed radiating materials with composite charring materials to evaluate their ablation and radiation properties for application to thermal protection for manned space vehicles
SPACECRAFT SHIELDING↗
SURVEY OF ATMOSPHERE RE-ENTRY GUIDANCE AND CONTROL METHODS
Guidance and control methods for spacecraft atmospheric reentry
CONTROL↗