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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 361 records · Page 20
All sourcesNASA NTRSDOE OSTI
NASA NTRS1980

Measurement of hydroxyl radical in the upper atmosphere using lidar from the Space Shuttle

The paper examines the measurements of hydroxyl radical in the upper atmosphere using lidar from the Space Shuttle. The measurement of the latitudinal and diurnal variation of OH would provide tests for stratospheric and mesospheric chemistry; two lidar systems aboard the Space Shuttle are described with the first providing the best signal to noise ratio for nighttime measurements at altitudes above 40 km, and the second giving a better performance during the day and at lower altitudes.

Heaps, W. S.↗
NASA NTRS1990

A facility for high resolution spectroscopy: Laboratory and ground based observations in support of upper atmospheric research

This research task consists of operating a facility for making spectroscopic observations in support of upper atmospheric research. The facility responds to the needs and interests of the visiting investigators. Therefore, the research objectives are not predetermined except in broad outline. The emphasis is on studies that take advantage of the particular strengths of the Fourier Transform Spectrometer on Kitt Peak: high spectral resolution combined with wide spectral range and low noise.

Brault, J. W.↗
NASA NTRS1978

Diffusion model for the upper atmosphere of Venus

On the basis of a linear theory it is shown that wind-induced diffusion associated with large-scale circulation in the Venus atmosphere leads to nighttime bulges in O, He, and H. The effect on He is very large with a 243-day rotation period of the atmosphere, yielding an upper limit for the maximum/minimum diurnal density ratio of approximately 1000. This ratio is much smaller for H (max/min of about 4) due to the greater importance of exospheric flow, which acts (as for He) as a damping mechanism. For the faster rotation period of 4 days consistent with the motions of the cloud tops, the diurnal variation of O is significantly reduced, contributing to an increase by a factor of two in the horizontal wind velocity. The same effect significantly reduces the He variations to an increase by a factor of 7 from day to night. The results suggest that composition and wind measurements provide valuable information on the rotation rate of the Cytherean thermosphere.

Mayr, H. G.↗
NASA NTRS1972

The composition of the upper atmosphere

Miniature mass spectrometers were developed and were carried on sounding rockets to determine the composition of the upper atmosphere. Techniques have been developed that accurately correct for the velocity and spin of the moving vehicle. Above 120 km N2, O2, and Ar appear to be in diffusive equilibrium. Most He concentration measurements show a more rapid decline with altitude than predicted by diffusive equilibrium. Because of the highly reactive nature of atomic oxygen, measurements of this species by mass spectrometry are low by an unknown factor.

Nier, A. O.↗
NASA NTRS1990

The interaction of an artificial electron beam with the earth's upper atmosphere - Effects on spacecraft charging and the near-plasma evironment

The ionization created in the earth's upper atmosphere by an electron beam emitted from a low altitude spacecraft is described by two coupled nonlinear differential electron transport equations for the up-going and down-going differential energy flux. The equations are solved numerically, yielding estimates of the differential electron energy flux density at the spacecraft location. At altitudes below 200-250 km and for beam energies around 1 keV, it is shown that secondary electrons supply a significant contribution to the return current to the spacecraft and thereby reduce the spacecraft potential. The numerical results are in good agreement with observations from the Charge 2 sounding rocket experiment.

Neubert, T.↗
NASA NTRS1990

Plasma density enhancements created by the ionization of the Earth's upper atmosphere by artificial electron beams

Analytical calculations and experimental observations relating to the interaction with the Earth's upper atmosphere of electron beams emitted from low altitude spacecraft are presented. The problem is described by two coupled nonlinear differential equations in the up-going (along a magnetic field line) and down-going differential energy flux. The equations are solved numerically, using the MSIS atmospheric model and the IRI ionospheric model. The results form the model compare well with recent observations from the CHARGE 2 sounding rocket experiment. Two aspects of the beam-neutral atmosphere interaction are discussed. First, the limits on the electron beam current that can be emitted from a spacecraft without substantial spacecraft charging are investigated. This is important because the charging of the spacecraft to positive potentials limits the current and the escape energy of the beam electrons and thereby limits the ionization of the neutral atmosphere. As an example, we find from CHARGE 2 observations and from the model calculations that below about 180 km, secondary electrons generated through the ionization of the neutral atmosphere by 1 to 10 keV electron beams from sounding rockets, completely balance the beam current, thereby allowing the emission of very high beam currents. Second, the amount of plasma production in the beam-streak is discussed. Results are shown for selected values of the beam energy, spacecraft velocity, and spacecraft altitude.

Neubert, Torsten↗
NASA NTRS1992

Titan's upper atmosphere - Structure and ultraviolet emissions

An analysis is conducted of the composition and thermal structure of Titan's upper atmosphere, and the relative importance of airglow-excitation processes, on the basis of Voyager 1 UV spectrometer data for solar occultation and airglow. Attention is also given to the Smith et al. (1982) optical depth profiles for the evening terminator, entrance occultation, and asymptotic temperature. A magnetospheric power input figure is obtained that is 25 times smaller than the initial estimate by Strobel and Shemansky (1982).

Strobel, Darrell F.↗
NASA NTRS1999

Studies of Excited Species in Planetary Upper Atmospheres

During the period of this portion of the on-going project, we investigated aspects of the upper atmospheres of Venus, Mars, Titan and Jupiter. During this period, we published four journal articles and one book chapter, copies of which are attached. The work reported in these manuscripts was in almost all cases begun under previous projects in the Planetary Atmospheres Program with the same title. I will summarize the papers, and another project that we worked on during this time period for which the papers will be published later.

Fox, J. L.↗
NASA NTRS1973

Wave-mean flow interactions in the upper atmosphere

The nature of internal gravity waves is described with special emphasis on their ability to transport energy and momentum. The conditions under which these fluxes interact with the mean state of the atmosphere are described and the results are applied to various problems of the upper atmosphere, including the quasi-biennial oscillation, the heat budget of the thermosphere, the general circulation of the mesosphere, turbulence in the mesosphere, and the 4-day circulation of the Venusian atmosphere.

Lindzen, R. S.↗
NASA NTRS1974

Surface /catalytic/ reactions on upper atmospheric aerosols

Highly reactive minor species and aerosol layers are present together at times in certain regions of the upper atmosphere. It is suggested that this interplay may lead to surface reactions that could affect the local photochemical balance. A simple model of the surface recombination of atomic oxygen at the mesopause, incorporating rough estimates of aerosol concentrations, is used to estimate the importance of this effect. Surface recombination does appear to be significant in comparison with gas phase recombination for atomic oxygen; however, major uncertainties remain in the model.

Olivero, J. J.↗
NASA NTRS1996

Calibration of the Microwave Limb Sounder on the Upper Atmosphere Research Satellite

The Microwave Limb Sounder (MLS) is a three-radiometer, passive, limb emission instrument onboard the Upper Atmosphere Research Satellite (UARS). Radiometric, spectral and field-of-view calibrations of the MLS instrument are described in this paper. In-orbit noise performance, gain stability, spectral baseline and dynamic range are described, as well as use of in-flight data for validation and refinement of prelaunch calibrations. Estimated systematic scaling uncertainties (3 sigma) on calibrated limb radiances from prelaunch calibrations are 2.6% in bands 1 through 3, 3.4% in band 4, and 6% in band 5. The observed systematic errors in band 6 are about 15%, consistent with prelaunch calibration uncertainties. Random uncertainties on individual limb radiance measurements are very close to the levels predicted from measured radiometer noise temperature, with negligible contribution from noise and drifts on the regular in-flight gain calibration measurements.

Jarnot, R. F.↗