Basic response relations for space vehicle attitude control using gyros.
Use of single-axis gyros for attitude control of space vehicles
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Use of single-axis gyros for attitude control of space vehicles
Investigation of standard suppression methods facilitates switching of inductively loaded circuits which causes interference in adjacent electronic equipment. The data are reduced to tabular form and rapid selection of components by the designer can be made without lengthy calculations or trial and error manipulations.
Definition and measurement of short term frequency stability - conference
Space science research at University of California at Los Angeles - magnetic shielded test facility, plasma studies, chemical effects of ionizing uv radiation, and 24 inch telescope
Space science at College of William and Mary - biology, infrared spectroscopy, and high energy physics
Transmission electron microscopy and X-ray diffraction observations of substructure and elastic strains in cold worked and annealed dispersion strengthened alloys
Contribution of hydrogen peroxide to electrode reaction in electrochemical cell by considering effect of catalyst on cell current
Space vehicle attitude control systems - manned space station, satellite in elliptic orbit, and solar perturbation of Mars Orbiter
Plasma potential, ion current density, and electron temperature and number density measurements for Hall current ion accelerator
Sensor requirements for spaceborne navigation, guidance, and control system for unmanned lunar landing vehicle
Physiological responses of monkeys subjected to prolonged periods of partial restraint
Equations for computing noise transmitted to space vehicle inside from random loading on outside
Truncated trigonometric functions for conic trajectory formulation in space flight applications
Erosion of blades and stators in steam turbines
Gas vortex stabilized arc radiation sources for solar simulation
Navigation and guidance principles and requirements - component technology, gyroscope application, inertial systems, specific force receivers, and geometrical aspects
Scientific satellite design considerations for spacecraft itself, spacecraft/launch vehicle interface, and ground support equipment and transportation
Heat transfer computer program description for spacecraft and satellite design