MINERALOGY OF THE OXIDATION PRODUCTS OF THE SPUTNIK 4 FRAGMENT AND OF IRON METEORITES
Comparison of oxidation products of the sputnik iv fragment after its reentry and those that occur in the crusts of iron meteorites
SPUTNIK IV SATELLITE↗
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Results for “REENTRY EFFECT”
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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Re-entry heating experiment to be flown by scout news release no. 64-202
Reentry heating experiment to be flown by scout launch vehicle to test ablating materials for use in apollo project flight
HEATING↗
Development of a rocketborne spectroradiometer to measure the radiation environment of a reentry vehicle.
Rocketborne spectroradiometer measurement of spectral radiation intensity of luminescent air in shock induced flow field produced by reentry vehicle
SHOCK SPECTRUM↗
Evaluation of materials in entry heating simulation
Facilities for simulating entry environment and response of ablative materials to simulated entry environment and flight tests
FLIGHT TEST↗
Nasa schedules project fire launch in may
Launching of Project FIRE spacecraft for reentry heating experiments
REENTRY EFFECT↗
Study of the stability and drag at mach numbers from 4.5 to 13.5 of a conical venus- entry body
Static and dynamic stability, and drag characteristics of conical nosed planetary vehicle during atmospheric reentry at escape velocity speeds
DYNAMIC STABILITY↗
Aerodynamic heating.
Aerodynamic heating of spacecraft during reentry, investigating characteristics for low density rarefied flow and high density continuum flow regimes
SPACECRAFT REENTRY↗
Factors influencing the design and performance of mars entry vehicles.
Hypervelocity heat transfer data and application to planetary entry of Mars and Venus
PLANETARY ENTRY↗
Flight reentry experiments.
Flight reentry research in terms of techniques used to investigate reentry environment, radio attenuation, materials behavior and observable phenomena
REENTRY EFFECT↗
Determination of parameters necessary for the prediction of ablative heat protection.
Ablative heat protection prediction of material response and environmental factors for ground- based test information
ABLATING MATERIAL↗
Thermochemical ablation.
Thermochemical interaction between ablation material and environment during manned reentry, using mainly graphite and composite materials
REENTRY EFFECT↗
High-resolution experimental spectra and theoretical studies of equilibrium radiation from a blunt body traveling at 37,000 ft/sec.
High resolution equilibrium radiation spectra for shock layer of blunt bodies at reentry velocities and radiative recombination of N and O ions
HIGH TEMPERATURE AIR↗
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↗
Equilibrium air radiation from shock layers at 11.3 km/sec.
High resolution equilibrium radiation spectra for shock layer of blunt bodies at reentry velocities and radiative recombination of N and O ions
HIGH TEMPERATURE AIR↗
Convective and radiative heat transfer during superorbital entry.
Convective and radiative heat transfer to reentry vehicles at superorbital velocities
RADIATIVE HEAT TRANSFER↗
Magnetogasdynamic re-entry phenomena.
MGD reentry flow regimes analyzed, noting increased bow shock standoff distance and drag, comparing in-flight and laboratory simulation
MAGNETOGASDYNAMICS↗
Impedance of plasma coated axial slot antenna
Plasma sheath effect on reentry communication system with slot antennas
Campbell, T. G.↗