An Update on the Long-Term Variations of Jupiter's Synchrotron Emission
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Engineering topics
Publications and source records attributed to Klein, M..
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Cycle life and kinetics studies were performed on sealed nickel metal hydride electrochemical cells with anodes of LaNi***4.7***Sn***sub0.3*** and of a standard misch metal alloy.
Changes to Jupiter's synchrotron radiation following the impact of Comet Shoemaker-Levy/9 are reported. Also, the consequences are reported for three possible mechanisms that might have caused those changes.
For the past twenty-three years the antennas of the NASA Deep Space Network have been used to measure temporal variations in Jupiter's decimetric flux density at 2295 MHz.
Load and stress recovery from transient dynamic studies are improved upon using an extended acceleration vector in the modal acceleration technique applied to structural analysis. Extension of the normal LTM (load transformation matrices) stress recovery to automatically compute margins of safety is presented with an application to the Hubble space telescope.
A K-band reflected-wave ruby maser was used on the 64-meter (DSS-43) antenna at the Tidbinbilla Tracking Station, near Canberra, Australia. Spectral line observations were carried out near 22 GHz for water vapor sources and near 24 GHz for ammonia sources. The water vapor observations were made in the direction of known southern OH and H2O maser sources. All of the previously detected water line sources examined were detected. In addition, two new water vapor maser sources were discovered, G301.1+1.1and G308.9+0.1. The spectrum of G301.0+1.1 is presented six ammonia sources were found: G291.3-0.7, G305.4+0.2, G322.2+0.6, G327.3-0.5, G333.6-0.2, and G268.4-0.8. Spectra of two of these sources, G291.3-0.7 (RCW 57) and G305.4+0.2, are presented. Both show clearly the presence of the quadrupole splitting satellite lines that will allow the determination of NH3 optical depths in these clouds.
The design and construction of nickel zinc cells, containing sintered nickel electrodes and asbestos coated inorganic separator materials, were outlined. Negative electrodes were prepared by a dry pressing process while various inter-separators were utilized on the positive electrodes, consisting of non-woven nylon, non-woven polypropylene, and asbestos.
Regions 2-deg x 2-deg in area centered on four spiral galaxies were scanned with the Goldstone 64-m antenna in search of satellite radio sources at 2295 MHz. Four control regions of equal area but free of galaxies brighter than 13th magnitude were also scanned. No significant excess in the number density of sources with flux densities greater than 0.10 Jy relative to the control fields was found. A detailed comparison is made between the results of this program and the results of previous investigators. In particular, attention is directed to the potentially important implications of an investigation by Tovmasyan (1968), who searched a large number of spirals and found evidence that a small percentage of them apparently have radio satellites located up to 20 arcmin from the central galaxy. Fifteen sources selected from Tovmasyan's list of 43 satellite sources were measured. The present results confirm his positions and relative flux densities for each of the sources.
Radio observations of Jupiter have been carried out at Goldstone, CA at a wavelength of 13 cm during the oppositions of 1969 and 1971. In 1969, circular-polarization and total-flux measurements were made with a 64-m radio telescope. From May through October 1971, Jupiter's flux density was measured at weekly intervals with a 26-m antenna. The upper limit to the degree of circular polarization over the longitude ranges 10-100 deg and 160-250 deg System III (1957.0) is 1%; the flux data have been used to derive a magnetospheric rotation period which is approximately 0.37 sec longer than the IAU System III (1957.0). The flux-density data define beaming curves which are apparently different from 11-cm beaming curves measured in 1964. Jupiter's peak flux density decreased by 20% between 1964 and 1971, and 8% between 1969 and 1971.
As exploration and utilization of space proceeds through the 1970s, 1980s, and beyond, spacecraft in earth orbit will become increasingly larger, spacecraft will travel deeper into space, and space activities will involve more complex operations. These trends require increasing amounts of energy for power and propulsion. The role to be played by nuclear energy is presented, including plans for deep space missions using radioisotope generators, the reactor power systems for earth orbiting stations and satellites, and the role of nuclear propulsion in space transportation.
Performance of prototype hydrogen oxygen electrolytic regenerative fuel cell stack with gas storage tank
Feasibility of metal oxygen primary batteries for multiple reserve use
Intermolecular potential function relation to individual macroscopic properties extended to simultaneous fit of all possible pair combinations
Statistical correlation between model intermolecular potential functions, and experimental properties
Search problems involving moving targets solved by using Markov decision models
Magnesium and aluminum electroforming process for solar concentrators