Study of local flow conditions over a hemispherically blunted 25 deg cone for a shallow re-entry trajectory
Local flow conditions over hemispherically blunted 25 deg cone for shallow reentry trajectory
BLUNT BODY↗
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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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Theoretical and Experimental Investigations of Spacecraft Antenna Problems in the Varied Operational Environments of Far-out-space and Atmospheric Re-entry Semiannual Report, 1 Jan. - 31 Jul. 1966
Spacecraft antenna, aperture, and reentry problems
ANTENNA↗
Magnetoaerodynamic re-entry.
Entry flight, relation between laboratory flows, in-flight conditions and MGD effects on flow field, drag and heat transfer
FLOW FIELD↗
Spacecraft transponder with re-entrant mode TWT amplifier.
Spacecraft transponder with reentrant mode TWT AMPLIFIER
TRANSPONDER↗
An alternate analysis of momentum deposition in the wake of a re-entry vehicle.
Momentum deposition in wake of reentry vehicle, discussing behavior of complex materials characterized by heat of ablation
MOMENTUM STORAGE↗
A re-analysis of the pilot eye-movement data.
Pilot eye movement data by recording eye fixations on flight instruments
AIRCRAFT INSTRUMENTATION↗
Re-association of hemocyanins from subunit mixtures.
Dissociation and reassociation reactions of hemocyanin mixtures analyzed by electron microscopy, noting original molecular structures
CHEMICAL REACTION↗
A re-examination of the crater near Crestone, Colorado.
Crestone crater morphology indicates that it is not meteoritic or cometary in origin
CRATER↗
Vacuum thermionic work functions of polycrystalline Nb, Mo, Ta, W, Re, Os, and Ir.
Vacuum thermionic work function for well-outgassed polycrystalline surfaces, noting techniques for accurate measurement of current, area and temperature values
METAL SURFACE↗
Including re-entry heating in rocket engine thermal analyses.
Reentry heat flux condition transformation into specified convective coefficients and temperatures, accounting for variation of flux with wall temperature
REENTRY CONDITION↗
A preliminary investigation of modified blunt 13 deg half-cone re-entry configurations at subsonic speeds
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REENTRY VEHICLE↗
The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13 Deg Half Cone at Mach Numbers to 0.90
Aerodynamic characteristics of blunt, lifting body reentry configuration
AERODYNAMIC CHARACTERISTICS↗
Stimulus-oriented Approach to Detection Re-examined
Effect of signal duration on detection in presence of continuous masking noise
CONTINUOUS NOISE↗
A Method for Determining Optimum Re-entry Trajectories
Determining optimum atmospheric reentry trajectories using Pontryagin maximum principle
PONTRYAGIN PRINCIPLE↗
Activation volume analysis for Cr and Cr-35 Re
Activation volume analysis for Cr and Cr-35Re
STRESS ANALYSIS↗
Use of the Langmuir probe to determine the electron density and temperature surrounding re-entry vehicles Final report
Shock tube tests of Langmuir probe for determining electron density and temperature surrounding reentry vehicle
ELECTRON DENSITY↗
Hypersonic nonequilibrium flow at re-entry of space vehicles and its thermodynamic relations
Hypersonic nonequilibrium flow at reentry of space vehicles and thermodynamic relations
THERMODYNAMIC PROPERTY↗