Generation of a plasma in a magnetic mirror geometry
Electron bombardment technique using thermally emitting cathode to produce plasma in magnetic mirror geometry
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Electron bombardment technique using thermally emitting cathode to produce plasma in magnetic mirror geometry
Geometry factors for solving thermal problems of satellites, and related computer procedure
Image dissector aperture geometries and scan patterns for use in star tracker systems
Space radiation shielding code for spacecraft geometry
Mean beam length with respect to band absorption laws and gas body geometries
Bounds for plane strain bulk modulus and shear moduli of multiphase fiber reinforced materials of arbitrary transverse phase geometry
Electron microscope method for measuring diffraction grating groove geometry in conjunction with fiber shadowing
Geometry of Earth magnetospheric tail and auroral electrojet current system and motions of low energy plasma
Correlation of interplanetary geometry with propulsion requirements for optimal low-thrust missions
Geomagnetic field geometry tables for trapped radiation and particles using scalar magnetic field intensity, invariant polar coordinants, and dipole moment
This paper describes a method for determining the optimum baffle configuration for suppressing excessive propellant sloshing in the tanks of a large launch vehicle. The optimum geometry for a baffle system is considered to be the one with the least mass which is capable of providing the necessary damping. The analysis considers a cylindrical tank and a baffle system made up of several flat ring baffles mounted horizontally. The basic assumptions are discussed and derivations given of the equations necessary to predict the optimum baffle configuration consistent with adequate strength. Numerical results are presented graphically, and some general conclusions are drawn.
Reaction geometry in oxidation and reduction of alkaline silver electrode
Computer programs for solving neutron and gamma transport and gamma heating problems in three- dimensional geometries
Aerodynamic characteristics of pyramidal reentry shapes with variable geometry, at subsonic speeds
Supersonic study of configuration geometry effects on pressure-coefficient and section normal-force- coefficient distributions for two-stage launch vehicle
Flow and pressure field analysis of parallel groove geometry for incompressible fluid with convective inertia effects
Relationship between photometric data and geometry of backscattering surfaces of moon
Interactions of magnetic materials using coupled films with closed flux geometry for use in magnetic memories