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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.

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At least 55 records · Page 3
All sourcesNASA NTRSDOE OSTI
NASA NTRS1975

Performance of DSS 13 26-m antenna at X-band

The X-band low-noise antenna (XLA) measurement feedcone was operated on the DSS 13 26-m antenna at Goldstone, California, during June 1975 to evaluate, primarily, the overall system efficiency. Radio sources were selected, commonly accepted values of flux density established, and measurements completed, and some conclusions were drawn. The antenna system presently suffers from poor pointing stability. On the other hand, the previously welded and rebolted main reflector has remained quite stable over a period of approximately 5 years.

Freiley, A. J.↗
NASA NTRS1975

DSS 14 X-band radar feedcone

A high-power 400-kW continuous-wave (CW) X-band radar feed system was described for use with the Goldstone, California, 64-m DSS 14 antenna system. Design considerations, their solutions, and final system testing are discussed. The radar system, unique in terms of antenna size, radiated power, and efficiency, became operational in December 1974.

Neff, D. E.↗
NASA NTRS1977

X-band atmospheric noise temperature statistics at Goldstone DSS 13, 1975 - 1976

X-band noise temperature data were taken at Goldstone DSS 13 for the period August 1975 through January 1977. A description of the experiment is given along with probability density functions for zenith noise temperature increase during all year quarters and day quarters. Elevation angle modeling of the data is described along with a discussion of the problems associated with relating wide beamwidth statistics to narrow beamwidth antennas.

Slobin, S.↗
NASA NTRS1977

DSS 13 automated antenna pointing subsystem phase 1 hardware

An automated antenna pointing subsystem (APS) is being installed at DSS 13 as part of the unattended station project. The function of the APS is to track an instructed position with the 26 meter antenna and to monitor the antenna servo system and meteorological conditions to ensure a proper operational environment. This article discusses the now-completed first phase of the digital hardware portion of the APS development.

Sievers, M. W.↗
NASA NTRS1977

Dual coupler configuration at DSS 14 for the Voyager era

A description is given of the dual coupler configuration which was installed at DSS 14 for station delay calibrations during the Voyager era. The Z correction values determined for these new and previous configurations are presented.

Otoshi, T. Y.↗
NASA NTRS1977

Radial bearing measurements of the 64-m antenna, DSS 14

The inspection fixtures and methods used to determine the extent of the aximuth radial bearing deformation at the 64 m DSS 14 are described. An annular separation developed between the circular steel runner and the grout, suggesting either failure of the grout or, as the case appears to be, stretching of the circular steel runner due to the formation of rust on the runner at the grout interface.

Gale, G.↗
NASA NTRS1978

Updated Z-corrections for 64-m DSS ground station delay calibrations

New Z-corrections which resulted from recent translator path delay calibrations made at DSS 14, 43, and 63 with newly developed DSN Portable Zero Delay Assemblies are presented. The test results indicate a successful transfer of technology from development to implementation and to the operations phase.

Otoshi, T. Y.↗
NASA NTRS1979

FTS maintenance and calibration at DSS 42/43

An FTS maintenance and calibration task was conducted at DSS 42/43 during August 1978. The objectives of this effort were (1) the routine maintenance and calibration of hydrogen masers, (2) installation and calibration of cesium standards, (3) installation of test equipment for frequency measurement, (4) CRG testing, (5) cabling inspection and repair, (6) check thermal and magnetic environment of H-maser/cesium room, and (7) calibration of frequency and timing subsystem.

Dachel, P. R.↗
NASA NTRS1979

DSS 13 antenna monitor system

The development of a monitor system for the DSS 13 antenna is presented. The system checks for accumulator pressures, differential pressures, wind velocity, power supplies, fluid temperatures, and fluid levels. It was concluded that the system performed properly in high winds and correctly reported all malfunctions.

Siev, B.↗
NASA NTRS1979

A prototype DSN X-S band feed: DSS 13 application

A prototype X-S band horn feed for future use at various DSN sites, dealing with the testing of the final fabricated feed at DSS 13 are discussed. Measured feedhorn patterns are presented, and efficiencies calculated. Preliminary results of system noise temperature and 26-m antenna system gain measurements are presented. Some measurements leading to an improved second generation feed are described. The results of the field measurements indicate that this horn will perform as originally specified and required. The tests for the second generation feed have indicated the potential cause of minor X-band moding.

Williams, W.↗
NASA NTRS1981

Development of a polymetric grout for the hydrostatic bearing at DSS 14

Results of an investigation into the causes of the deterioration and premature failure of the grout under the hydrostatic bearing runner at DSS 14 are reported. Generic types of materials were screened and tested to find a grout material more resistive to the causes of grout failure. Emphasis was placed on the physical properties, strength, modulus of elasticity, and resistance to erosion and chemical attack by oil and unique requirements imposed by each material for mixing, placing, compacting, and cooling. The polymetric grout developed to replace the dry grout is described.

Mcclung, C. E.↗
NASA NTRS1982

Maintenance and operations tasks accomplished at DSS 12 during the antenna panel replacement downtime

The heavy schedule of tracking activities at the Echo Deep Space Station (DSS 12) prevents some time-consuming maintenance tasks from being performed. Careful coordination prior to and during a mandatory task (antenna panel replacement) made it possible to do a large number of unrelated tasks that ordinarily would have to be deferred. The maintenance and operations tasks accomplished during the downtime are described.

Butcher, L.↗
NASA NTRS1982

Potential availability of diesel waste heat at Echo Deep Space Station (DSS 12)

Energy consumption at the Goldstone Echo Deep Space Station (DSS 12) is predicted and quantified for a future station configuration which will involve implementation of proposed energy conservation modifications. Cogeneration by the utilization of diesel waste-heat to satisfy site heating and cooling requirements of the station is discussed. Scenarios involving expanded use of on-site diesel generators are presented.

Hughes, R. D.↗
NASA NTRS1983

Energy consumption analysis of the Venus Deep Space Station (DSS-13)

This report continues the energy consumption analysis and verification study of the tracking stations of the Goldstone Deep Space Communications Complex, and presents an audit of the Venus Deep Space Station (DSS 13). Due to the non-continuous radioastronomy research and development operations at the station, estimations of energy usage were employed in the energy consumption simulation of both the 9-meter and 26-meter antenna buildings. A 17.9% decrease in station energy consumption was experienced over the 1979-1981 years under study. A comparison of the ECP computer simulations and the station's main watt-hour meter readings showed good agreement.

Hayes, N. V.↗
NASA NTRS1984

X-band Uplink Technology Demonstration at DSS-13

The status of the X-band uplink development program is examined from a systems' viewpoint. The hardware, designed and built under the program, is now in place at DSS-13. System stability testing is underway. An X-band receive capability is being implemented on both the Galileo and the Venus Radar Mapper spacecraft. Experiments are planned to demonstrate the capabilities of the X-band uplink system and to permit performance of the gravitational wave experiment on the Galileo orbiter and obtain a more detailed gravity map of Venus.

Meeker, J. G.↗
NASA NTRS1984

DSS 13 Microprocessor Antenna Controller

A microprocessor based antenna controller system developed as part of the unattended station project for DSS 13 is described. Both the hardware and software top level designs are presented and the major problems encounted are discussed. Developments useful to related projects include a JPL standard 15 line interface using a single board computer, a general purpose parser, a fast floating point to ASCII conversion technique, and experience gained in using off board floating point processors with the 8080 CPU.

Gosline, R. M.↗