Free oscillations of circular conical and cylindrical shells reinforced by rigid circular ribs
Free axially asymmetric oscillations of conical and cylindrical shells reinforced by circular ribs
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Free axially asymmetric oscillations of conical and cylindrical shells reinforced by circular ribs
Magnetic stabilizing and attitude control of rotating satellite in circular earth orbit
Cold cathode ionization gage in a stainless steel housing accurately measures high pressures. The penning effect is used with a high voltage discharge in the presence of a magnetic field for an ion current proportional to the gas pressure in the gage.
Cosmic ray deflections in geomagnetic field, variational coefficients, and diurnal intensity variations - tables
Dosimetric interpretation of flux/rigidity spectra for solar flare corpuscular radiation
Design of control deflections and structural loads of space vehicle for flight stability through atmospheric disturbances
Test for stiffness of fabrics used to measure flexural stiffness of thin plastic films and metal-plastic laminates for spacecraft application
Space vehicle flight control modes for basic wind profiles - reduction of aerodynamic loads for wind, wind shear, and gust conditions
Lightweight ceramic foam for thermal insulation heat shields of launch structures
Stationary rotation of stars based on law of solar rotation
Minimum fuel control of spacecraft in orbit using extended method of steepest descent
Stress field generation by screw dislocation pile- up at hard circular cylindrical inclusions obtained, using approximation of continuously distributed dislocations
Molecular pair distribution function in perfect crystalline solids, using method based on cell cluster theory
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Matrix of manganese-alumino-silicate glass simplifies the processes of metallizing alumina ceramics. Because the manganese in the glass is preoxidized to the 2 plus state by firing in nitrogen, the ceramic can be metallized in dry hydrogen. Lengthening the firing time permits a lower metallizing temperature.
Digital program for dynamics of nonrigid gravity gradient satellites
Liapunov stability derived from kinetic energy and squared angular momentum