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Andrews, J. C.

Publications and source records attributed to Andrews, J. C..

10 records
All sourcesNASA NTRSDOE OSTI
NASA NTRS1992

Electric propulsion - The future is now

A comprehensive development status evaluation is presented for the field of electric propulsion. Specific impulses range from 500-800 sec for satellite stationkeeping and 800-1500 sec of earth-earth orbit-raising maneuvers to 2000-5000 sec for trajectories to Mars and as much as 5000-100,000 sec for trajectories to more distant destinations. The successful deployment of low-power arcjet systems for auxilliary propulsion has been critical to the development of designs for higher-performance devices.

Turchi, Peter J.↗
NASA NTRS1982

High resolution satellite observations of mesoscale oceanography in the Tasman Sea, 1978 - 1979

Of the Nearly 1000 standard infrared photographic images received, 273 images were on computer compatible tape. It proved necessary to digitally enhance the scene contrast to cover only a select few degrees K over the photographic grey scale appropriate to the scene-specific range of sea surface temperature (SST). Some 178 images were so enhanced. Comparison with sea truth show that SST, as seen by satellite, provides a good guide to the ocean currents and eddies off East Australia, both in summer and winter. This is in contrast, particularly in summer, to SST mapped by surface survey, which usually lacks the necessary spatial resolution.

Nilsson, C. S.↗
NASA NTRS1980

Internal electrostatic discharge hazard risk assessment to the Galileo orbiter

A worst case assessment was performed on the Command Data System (CDS) multilayer printed circuit board and an output power transformer module in the power subsystem. An estimate of the Jovian environment during the 35 hour orbit insertion was supplied by JPL and used as an input to calculate the electron transport into the Galileo components. A radiation shielding analysis computer code, CHARGE, calculated the electron transport deposition trapped in the anticipated sensitive areas of the multilayer board and transformer module. Based on these trapped charge calculations electric fields were calculated between the identified isolated areas and the spacecraft ground. The results of the assessment of electrostatic discharge (DSD) in the CDS multilayer printed circuit board indicate that the probability of ESD in the FR4 is low. The probability of ESD in the components attached to the multilayer board, however, is uncertain based on a lack of prior experimental data.

Schmidt, R. E.↗
NASA NTRS1980

Heat Capacity Mapping Mission

The Tasman Front was delineated by airborne expendable bathythermograph survey; and an Heat Capacity Mapping Mission (HCMM) IR image on the same day shows the same principal features as determined from ground-truth. It is clear that digital enhancement of HCMM images is necessary to map ocean surface temperatures and when done, the Tasman Front and other oceanographic features can be mapped by this method, even through considerable scattered cloud cover.

Nilsson, C. S.↗