Failure analysis of Delron inserts in the 60B20217-2 heat shield panel
Failure analysis of Delron inserts in 60B20217-2 heat shield panel
Teeter, L. W.↗
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Results for “SHIELDING”
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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Vacuum thermal conductivity measurements of NASA E4A1 elastomeric heat shield material
Line source vacuum thermal conductivity measures for elastomeric heat shield material
Comparin, R. A.↗
Nuclear reaction cross sections for spacecraft shield design
Nuclear reaction cross section data for spacecraft shield design, and for determining radiation dose effect on astronauts
Peelle, R. W.↗
Nonlinear stability analysis of Apollo aft heat shield
Nonlinear structural analysis of stress and buckling pressures of aft heat shield of Apollo spacecraft
Stricklin, J. A.↗
Some uses of discrete ordinates codes for shielding analysis at NASA, Lewis Research Center
Discrete ordinates codes used to determine secondary gamma sources in reactor assemblies and shields
Lahti, G. P.↗
Flight test analysis of Apollo heat shield material using the Pacemaker vehicle system
Ablation and temperature data for Apollo heat shield material using Pacemaker vehicle for flight test
Graves, R. A., Jr.↗
Thermal design of inflatable spherical shadow shields
Heat transfer from balloon type shadow shield to cryogen storage tank - mathematical discussion
Campbell, J. P.↗
Flight investigation of the effects of Apollo heat-shield singularities on ablator performance
Launch vehicle flight tests of effects of Apollo heat shield irregularities on ablative material performance
Ohare, B. J.↗
Entry length for the rocket meteorological radiation shield
Thermal entry length of temperature sensor placement in tubular radiation shield
Alsaji, S.↗
Heat shield instrumentation - Development and evaluation
Methods and techniques for monitoring critical heat shield parameters during spacecraft reentry
Hicks, E. W., Jr.↗
A study of the effects of environmental and ablator performance uncertainties on heat shielding requirements for blunt and slender hyperbolic-entry vehicles.
Environmental and ablator performance uncertainties effects on heat shielding requirements for blunt and slender hyperbolic entry vehicles
Coleman, W. D.↗
Thermal design of inflatable spherical shadow shields.
Heat transfer from inflatable spherical balloon shadow shield to spherical cryogen storage tank, noting several design factors and extensions of previous work
Campbell, J. P.↗
Shielding of solar cells against Van Allen belt protons.
Satellite solar cell life in Van Allen belt proton flux predicted as function of shielding thickness by computer program
Carosella, C. A.↗
Inverse third power law for the shielding of test particles.
Far field effective potential of charged particle in Vlasov plasma, discussing inverse third power law for shielding test particles
Joyce, G.↗
Radiation damage shielding of solar cells on a synchronous spacecraft.
Silicon solar cells radiation damage shielding on ATS 1 synchronous spacecraft
Waddel, R. C.↗
Effects of environmental and ablator performance uncertainties on heat-shielding requirements for hyperbolic entry vehicles.
Environmental and ablator performance uncertainties effects on heat shielding requirements for blunt and slender hyperbolic entry vehicles
Coleman, W. D.↗
Synthesis of calculational methods for design and analysis of radiation shields for nuclear rocket systems
Eight computer programs make up a nine volume synthesis containing two design methods for nuclear rocket radiation shields. The first design method is appropriate for parametric and preliminary studies, while the second accomplishes the verification of a final nuclear rocket reactor design.
Capo, M. A.↗
Self-shielding printed circuit boards for high frequency amplifiers and transmitters
Printed circuit boards retaining as much copper as possible provide electromagnetic shielding between stages of the high frequency amplifiers and transmitters. Oscillation is prevented, spurious output signals are reduced, and multiple stages are kept isolated from each other, both thermally and electrically.
Galvin, D.↗