The magnetic field geometry of Jupiter and its relation to Io modulated Jovian decametric radio emission
Jovian magnetic field geometry and Io modulated decametric radio emission
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Jovian magnetic field geometry and Io modulated decametric radio emission
Variable geometry manned orbital vehicle having high aerodynamic efficiency over wide speed range and incorporating auxiliary pivotal wings
Developing empirical equation for calculating effects of container geometry on liquid lubricant evaporation in vacuum
Computer program to generate turbine aerodynamic requirements, approximate external blade geometries, and coolant flow requirements for two stage axial flow turbine
Booster wing geometry effects on space shuttle design requirements
Inlet nozzle geometry effects on subsonic flow characteristics of miniature total pressure tubes including pitot tube static and dynamic pressure and flow velocity measurements
Low speed wind tunnel test on effects of horizontal tail geometry on longitudinal stability of orbiter shuttle
Low speed wind tunnel tests on effects of vertical tail and geometry on directional stability of orbital space shuttle model
Noise reduction studies involving variable geometry inlet guide vanes for choking using two-sector cascade apparatus with three inlet configurations
Unfurlable spacecraft antenna design and electrical characteristics, using Gregorian geometry with conical main and parabolic subreflector
Light scattering geometry from infinite cylinder shown consistent with Rayleigh-Gans formalism
Transferred electron bulk negative differential conductivity devices, analyzing combined doping and geometry effects on space charge and domain dynamics
Rocket engine propellant injectors with noncircular orifice geometry, presenting experimental spray patterns and predicted performance for noncircular and circular orifice configurations
Jupiter magnetic field geometry related to Io modulated Jovian decametric radio emission
Wake model and computer program to compute geometries, flows and velocity influence coefficients for helicopter blade load calculations
Canard space shuttle reusable launch vehicle wing geometry variations effect on flyback systems weight, noting influence of aspect ratio and wing area
Jupiter atmospheric probe using relay-link communications geometry between probe and flyby spacecraft for 3.5 hr intervals
The theory used in FASTER-III, a Monte Carlo computer program for the transport of neutrons and gamma rays in complex geometries, is outlined. The program includes the treatment of geometric regions bounded by quadratic and quadric surfaces with multiple radiation sources which have specified space, angle, and energy dependence. The program calculates, using importance sampling, the resulting number and energy fluxes at specified point, surface, and volume detectors. It can also calculate minimum weight shield configuration meeting a specified dose rate constraint. Results are presented for sample problems involving primary neutron, and primary and secondary photon, transport in a spherical reactor shield configuration.