Studies of ion-neutral reactions by a photoionization mass-spectrometer technique. I.
Photoionization mass spectrometer for ion-molecule reaction studies, determining ion residence times, drift velocities, diffusion coefficients and ion temperatures
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Photoionization mass spectrometer for ion-molecule reaction studies, determining ion residence times, drift velocities, diffusion coefficients and ion temperatures
Photoionization mass spectrometer for charge transfer reaction analysis
Charge exchange cross sections measurements for ion-molecule pairs of hydrogen, argon, krypton, helium and xenon
Atom and ion desorption energy, chemisorption theory and surface bonds, work functions and potential energy in literature review of adsorption on metal surfaces
Beam-foil technique of exciting electronic levels in atoms and ions applied to Al and Fe
Cross sections computed for excitation and ionization of atoms and ions by electrons, using peaking approximation to evaluate Coulomb-Born matrix approximation
Simultaneous solution of continuity and heat conduction equations for ionospheric plasma consisting of electrons, atomic O ions and neutral gas species, discussing varying solar flux effects
Internal energy partition function of atom or ion immersed in plasma - astrophysical application
Radiative lifetime for atomic transitions in UV multiplets of zinc and cadmium atoms and ions measured using phase shift method
Positive atomic oxygen ion reactions with carbon dioxide detected using ion cyclotron and double resonance methods
Ionized magnesium dayglow measurement in sporadic E layer by rocket-borne UV spectrometer, determining ion to atom ratio
Electro-optical system for measuring very small Doppler shift displacements of spectral wavelengths emitted by atoms and ions in high velocity plasma beam is discussed. Operation of circuits is described and circuit diagram is included.
The ATS-F satellite will carry two cesium ion thrusters. Cesium is a material that is not present in the upper atmosphere, and there is concern that the introduction of this material may result in some unexpected behavior. A study has been conducted to assess the magnitude of the effects that are to be expected. No observable effects were found as a result of the study. Consideration was given to the origin and destination of the material and the various reactions that could occur. The origin was considered to be anywhere in space from altitudes of about 100 km upward. The probable short term destination is in the form of cesium ions trapped in the earth's magnetic field or as ions and atoms in the heterosphere. The maximum possible number of cesium atoms in the field of view of an earth based observer is of the order of one million per square centimeter, far too few to be observable by visible, near-visible, or radio-frequency means. Further, no phenomena could be found that would result in the occurance of an observable event.
Reactions between atoms and ions of the interstellar medium and vibrationally excited molecular hydrogen are shown to produce a specific set of molecules. Molecules such as CO and CN can readily be produced in abundances greater than those of corresponding hydrides. When quantified in a simple manner the equilibrium density of molecules compares well with the observed values for the star Oph.
The drag coefficients for the Echo 1 and Explorer 24 spherical surfaces in an O environment were experimentally determined over an energy range of 4 to 200 eV. The experiment was performed by generating a beam of atomic oxygen ions of the proper energy, neutralizing a portion of the beam, and then allowing only the neutral O particles to strike a very sensitive torsion balance. The momentum transferred to the surface was determined from the deflection of the torsion balance. At the lower energies, the more intense ion beam had to be used instead of the neutral beam. The drag coefficients are found to be slightly greater than 2 at energies corresponding to satellite velocities.
The formation of the classical interstellar molecules CH, CH(+), and CN is investigated, giving attention to the chemistry of moderate-density interstellar clouds. An H I region is considered in the model employed in the study. The major constituents in the region are atoms or ions because of the intensity of the UV radiation field. Aspects of radiative association are discussed together with chemical reactions, the electronic states and optical properties of CH and CH(+), and photodissociation rates.
This paper describes the development and integration of a one millipound thrust ion thruster system on the NASA Goddard ATS-F spacecraft with the objective of outlining for the propulsion system engineer: (1) system interactions or potential problems associated with the application of ion thruster systems, and (2) progress which has been made and is being made in identifying and solving these problems. Principal areas of concern are the compatibility of the thruster exhaust (ions and atoms) with sensitive spacecraft surfaces and possible electromagnetic interactions of the thruster and its exhaust with other spacecraft subsystems.
Auroral optical measurements made aboard NASA's CV 990 were analyzed. The measurements analyzed form a small part of extensive spectroscopic, photometric and photographic data gathered during the 1968 and 1969 Airborne Auroral Expeditions. Simultaneous particle measurements from ESRO IA satellite were used in the analysis. Information about magnetospheric boundaries, interaction between magnetosheath particles and the terrestrial ionosphere, the polar bulge in helium abundance and excitation mechanisms of the triplet state of atmospheric N2 in auroras was obtained. Further analysis of the data is required to elucidate the relation between 3466 and 5200 A emissions of NI and the excitation of 3726-3729 A emissions from atomic oxygen ions in auroras.