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Dunne, J. A.

Publications and source records attributed to Dunne, J. A..

At least 19 records
All sourcesNASA NTRSDOE OSTI
NASA NTRS1989

Testing general relativity with Landers on the Martian satellite Phobos

A planned experiment to obtain range and Doppler data with the Phobos 2 Lander on the surface of the Martian satellite Phobos is described. With the successful insertion on January 29, 1989 of Phobos 2 into Mars orbit, it is anticipated that the Lander will be placed on the surface of Phobos in April 1989. Depending on the longevity of the Lander, range and Doppler data for a period of from one to several years are expected. Because these data are of value in performing solar-system tests of general relativity, the current accuracy of the relevant relativity tests using Deep Space Network data from the Mariner-9 orbiter of Mars in 1971 and from the Viking Landers in 1976-1982 is reviewed. The expected improvement from data anticipated during the Phobos 2 Lander Mission is also discussed; most important will be an improved sensitivity to any time variation in the gravitational 'constant' as measured in atomic units.

Anderson, J. D.↗
NASA NTRS1984

Planetary spacecraft as optical instrument platforms

The pointing system, telemetry rate, thermal control, power, command, and available mass of planetary spacecraft are described. A comparison of the pointing and stability capabilities of the three-axis stabilized spacecraft and the spin stabilized spacecraft is presented. The development of a hybrid spacecraft, which combines the spin and three-axis design, is examined. The attitude control and articulation system, and the instruments of the Galileo, a hybrid spacecraft, are analyzed.

Vescelus, F. E.↗
NASA NTRS1982

Observational parameters for remote sensing in the next decade

The spectral and spatial requirements for remote sensing in the next decade are presented. The requirements presented were obtained through extensive literature research and discussions with leading members of the various remote sensing research communities. In the 0.35-2.5 micron region of the spectrum, numerous bands will be needed at bandwidths as narrow as 10-20 nanometers. There is also growing interest in the thermal infrared (8-14 microns). Spatial resolution (instantaneous field of view) of 5 to 10 meters will be of great benefit to many fields of remote sensing.

Vane, G.↗
NASA NTRS1980

Seasat performance evaluation - The first two steps

Seasat, the satellite dedicated to the study of the oceans using microwave sensors, collected a data set containing information on sea surface winds, sea surface temperatures, wave heights, wave directions, internal waves, currents, tides, the marine geoid, and atmospheric water content. The first two steps of the performance evaluation of the satellite have been completed: (1) the engineering assessment and (2) the sensor evaluation. The results are encouraging for the performance of the instruments and the first level of data processing algorithms.

Lame, D. B.↗
NASA NTRS1980

SEASAT-SAR data analysis in the US: An update

A graph is shown which compares SEASAT synthetic aperture radar (SAR) wave length measurements and Krasman's shallow water dispersion relationship for a swell system of deep water length 210 m and period 11.7 sec. The data were taken during the Duck experiment. The status of the production of optically correlated SAR data is given along with a tabulation of both digitally and optically processed SAR image data available to the user community as of Aug. 1979. Results from several SAR workshops are mentioned.

Dunne, J. A.↗
NASA NTRS1979

Seasat mission overview

The microwave oceanographic satellite Seasat is described, and the main characteristics of its five sensors, including a radar altimeter, the Seasat-A scatterometer system, a synthetic aperture radar, a visual and infrared radiometer, and a scanning multichannel microwave radiometer, are discussed. Experimental programs undertaken by the satellite are briefly summarized.

Born, G. H.↗
NASA NTRS1979

The mission of Seasat-A

The experimental oceanographic satellite Seasat-A produced microwave observations of the world's oceans for some three months in the summer of 1978. Study of a small set of the data collected at a time and in the area of intensive conventional surface observations have shown that the technology represented by this satellite can provide useful information on waves, winds and sea surface temperature on a global scale. Further analysis is required to quantitatively assess the potential contribution of satellite height and orbit determination to the study ocean dynamics, but early results are quite encouraging.

Dunne, J. A.↗
NASA NTRS1978

The experimental oceanographic satellite Seasat-A

The experimental Seasat-A satellite, scheduled for launch in 1978, is designed to provide measurements of sea-surface temperature, surface wind speed and direction, sea state and directional wave spectra. The instrument package of the satellite includes a highly precise radar altimeter, a wind-field scatterometer, a synthetic-aperture imaging radar, a scanning multifrequency microwave radiometer and a radiometer operating in the visual and infrared. Tides, currents and storm surges on the marine geoid may be monitored through analysis of range information from the radar altimeter and a satellite ephemeris; sea-ice reconnaissance is also planned.

Dunne, J. A.↗
NASA NTRS1977

Seasat-A data acquisition and distribution

The instrument package of the Seasat-A satellite, scheduled for launch in 1978, consists of a short-pulse radar altimeter, a wind field scatterometer, a scanning multichannel microwave radiometer, and an experimental L-band synthetic aperture radar. Objectives of the mission include precision altimetry for marine geoid and sea surface topography assessments, the determination of wave directional spectra through radar scatterometry, and sea surface temperature measurements through microwave emission analysis. The synthetic aperture radar, operated selectively, is intended to yield land and sea imagery with a resolution of 25 m for such requirements as coastal surveys.

Dunne, J. A.↗
NASA NTRS1976

Mariner 10 observations of Mercury

The paper reviews Mariner 10 observations of Mercury during the three encounters in March 1974 in a darkside passage at an altitude of 703 km, in September 1974 in a brightside passage at southern latitudes at a distance of some 50,000 km, and in March 1975 in another darkside passage at midnorthern latitudes at a closest approach distance of about 327 km. Evidence for the chemical differentiation of Mercury is found in the morphology and distribution of the smooth plains. The concept of chemical differentiation is shown to be consistent with the observation of global compression in that the crustal shortening observed could readily be explained by a phase change in a large metal-rich core. Extreme ultraviolet observations set an upper limit to the atmosphere at around one trillionth bar, with positive identification of a tenous (10 to the minus 15th bar) He atmosphere. An unexpected finding during the first encounter was the existence of a planet-related magnetic field. The third encounter yielded unequivocal evidence that the field is of internal origin, providing an independent line of evidence that Mercury possesses a large metal-rich core.

Dunne, J. A.↗
NASA NTRS1976

The Seasat-A project - An overview

Scheduled for launch in the second quarter of calendar year 1978, the Seasat-A satellite is designed to provide all-weather global monitoring of sea surface temperature, significant wave height, surface wind speed and direction and departures from the marine geoid corresponding to ocean dynamic processes. These data will be obtained from an array of microwave instruments, two active ones (short pulse radar altimeter and wind field scatterometer) and one passive (scanning multichannel microwave radiometer). An experimental L-band synthetic aperture radar, operated on a selected basis for approximately four percent of the time, will provide land and ocean images with a resolution of 25 meters and a swath width close to 100 km for the study of coastal processes, sea ice and ocean wave characteristics. The mission objectives focus on an evaluation of the performance of the instruments in terms of their capabilities to characterize the desired geophysical quantities and the utility of such measurements to the study and exploitation of the world's oceans.

Dunne, J. A.↗
NASA NTRS1975

The Mariner 10 Venus encounter - A review

A brief description is given of the Mariner 10 spacecraft, its complement of scientific instruments, and its encounter with Venus. It is noted that the geometry of the Venus encounter was dictated entirely by the necessity to use Venus' gravitational field to deflect the flight path toward Mercury. Results discussed include observations of plasma and magnetic-field perturbations several hundreds of Venus radii downstream of the solar wind which indicated the presence of a well-developed plasma tail and UV observations of H, He, C, and O abundances in the upper atmosphere. The atomic-oxygen abundance was found to be an order of magnitude higher than that observed on Mars. Radio-occultation measurements showed four distinct temperature inversions in the atmosphere and two nightside ionospheric layers. Results of television observations are also discussed which confirmed the hazy model of the visible atmosphere.

Dunne, J. A.↗
NASA NTRS1974

Mariner 10 Mercury encounter

Mariner 10's closest approach to Mercury on Mar. 29, 1974 occurred on the dark side of the planet at a range of approximately 700 kilometers. The spacecraft trajectory passed through the shadows of both the sun and earth. Experiments conducted included magnetic fields, plasma and charged particle studies of the solar wind interaction region, television photography, extreme ultraviolet spectroscopy of the atmosphere, the detection of infrared thermal radiation from the surface, and a dual-frequency radio occultation in search of an ionosphere.

Dunne, J. A.↗
NASA NTRS1974

Mariner 10 Venus encounter

Review of the scientific objectives of the Mariner 10 mission with regard to observations of Venus during a flyby, and description of the equipment installed on the spacecraft to fulfill these objectives. A detailed description is given of the hardware modifications made to the payload specifically for the Venus sequence. In discussing the encounter operations, two spacecraft problems which significantly affected the Venus encounter sequence are cited - namely, a failure of the television optic heaters to come on shortly after launch, and the occurrence of a roll gyro oscillation.

Dunne, J. A.↗