Effects of Solar Angle of Incidence on Intramodular Photovoltaic Irradiance Uniformity.
Abstract not provided.
SEARCH · Search NASA
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Abstract not provided.
Abstract not provided.
Explore the source record for details and available documents.
Solar plasma and electromagnetic radiation on thin films and surfaces
Explore the source record for details and available documents.
Solar radiation shield for thermal control of spacecraft subjected to large changes in solar energy
Explore the source record for details and available documents.
Explore the source record for details and available documents.
Solar phenomena analysis associated with polar cap absorption events from solar flare protons for prediction space radiation conditions
Second order theory for trajectories near lunar libration point based on four body model including sun, earth, moon, and satellite
Gyro-synchrotron radiation intensity, spectrum, and polarization calculations from magnetoactive plasma electron distribution
Simulated Martian environmental conditions for performance tests of solar cells
Subjection of solar cell assemblages to simulated lunar dust storms in wind tunnels
Thermal cycling tests of bent solar cell interconnection tabs on OAO module
Current estimates of solar-electric-propulsion spacecraft performance are based upon a solar-array output power which is degraded by approximately 10-13% to account for possible losses caused by proton, electron and micrometeorite damage. Past studies have used a worst case analysis in which the maximum degradation was taken to occur at the beginning of the mission. This paper presents a comparison of mission studies using a hypothetical exponential decrease in power with time, with those using a sudden degradation of solar power. These comparisons indicate that the performance gain by using a time varying degradation during the mission is quite small for outbound missions in the solar system. In addition an indication of the power allocation strategy to be followed during a mission is presented.
Explore the source record for details and available documents.
The stability of the low-frequency waves propagating transverse to the magnetic field of a plasma composed of electrons, protons, and alpha particles with anisotropic electron and ion temperatures is explored. The threshold for the ordinary mode instability and the growth rates have a very strong dependence on the electron temperature anisotropy but have a comparatively weaker dependence on the ion temperature anisotropy, on the relative abundance of helium to hydrogen, and on the relative streaming of two ion species. The threshold for the instability of these low-frequency waves is (m sub e/m sub p) to the 1/2 power times smaller than the one corresponding to high-frequency waves; however, for a relative abundance of helium to hydrogen up to 20% for the relevant known magnetic fields, particle densities, temperatures, and drifts, the solar wind remains below the threshold for this instability.