Development of nondestructive testing techniques for honeycomb heat shields Annual report, 1 Jul. 1965 - 31 May 1966
Nondestructive testing techniques for Saturn honeycomb heat shields
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Nondestructive testing techniques for Saturn honeycomb heat shields
Charged particle radiation shielding characteristics of magnetic fields generated by solenoids
Stagnation point velocity and pressure distribution over heat-sink shielded reentry vehicle to test boundary layer heat transfer theories
Astronauts with thin shielding in radiation exposure from heavy nuclei in solar particle beams
Dipole matrix elements for helium in first order shielding approximation as function of screening parameter
Lightweight inflatable shadow shields for cryogenic space vehicles and performance in conjunction with superinsulation
Gravitational shielding and absorption, examining tidal effects induced in solid sphere by another sphere, analogy to electromagnetic fields, etc
Liquid nitrogen-cooled shield against oil vapor contamination of proton accelerator in vacuum chamber
Self-sealing shield for protection of micrometeorite penetration in propellant tank
Radiation hazards of interplanetary space and related shielding problems
Characterization and reproducibility of nylon phenolic resin syntactic foam for use in ablative heat shields of Scout vehicle nosecaps
Development of nondestructive testing system, using ultrasonic techniques, for detecting disbonds in composite honeycomb heat shields of Saturn launch vehicle
Optical reflectance measurements of pyrolytic graphite and phenolic nylon chars and potential application to heat shield requirements
Bibliography of computer codes on radiation and nuclear shielding
Literature and industrial surveys of nondestructive testing equipment and techniques for application to honeycomb heat shields, including partially annotated bibliography
Feasibility of programmed heat shield for temperature and power control for spacecraft on-board power
Structural analysis of Apollo aft heat shield under water impact loading conditions
Lightweight ceramic foam for thermal insulation heat shields of launch structures