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Neutral material.

The release of neutral material into the space environment has been performed for many years under the general heading of chemical releases. The purposes of these releases have been primarily to use the material as a tracer for the study of winds, local electric fields or to initiate gas/plasma chemistry in the upper atmosphere. Observation of these phenomena is often accomplished by optical measurements of light emissions from the released material. The initially neutral material is induced to emit light as a result of excitation or ionization by solar ultra violet radiation or by exceeding a critical velocity relative to the background plasma called the Critical Ionization Velocity (CIV). Intensity maps show the location of the gas cloud, and velocities can be obtained by tracking or by using interferometers to measure Doppler shifts of known emission lines of the released material. Once the neutral material is ionized it is subject to forces by local electric fields causing plasma drift velocities related to the local electric and magnetic field vectors. The contaminant material also affects the chemical balance in the upper atmosphere, and can have dramatic effects on the local ionospheric plasma density. The resulting changes in plasma density can be observed either optically or by radio sounding of the ionosphere at the injection volume, and occasionally by in situ probes placed into the reaction volume by rockets or satellites. More insight into the plasma physics of the interaction can be obtained by measuring waves generated in the interaction region.

In recent years, neutral releases have also been used specifically to study the CIV effect which has been postulated to occur when the component of the relative velocity between a gas and a background plasma which is perpendicular to the local magnetic field exceeds the speed corresponding to the kinetic energy of the gas molecules being equal to the ionization potential of the gas. This inequality can be satisfied at sounding rocket speed for heavy gases or at orbital speeds for lighter gases, or the gas can be ejected from a container at high speeds as in shaped charge experiments.

Several active experiments involving the release of gas have occurred in the last four years. The Combined Release and Radiation Effects Satellite (CRRES) released quantities of vaporized barium, strontium and calcium into the magnetosphere at geocentric distances of between 2.0 and 6.2 earth radii and also into the upper atmosphere at 450 km altitude at low latitudes in 1991 (Huba et al., 1992a, 1992b). The CRRES studies have added considerably to our knowledge of the interaction of plasma with the space environment at high and low altitudes. The formation of magnetic cavities has been observed at high altitudes, and also the polarization field is sufficient for cross-field motion of the plasma for a few seconds until the density drops to a low value and the field weakens. Associated with the dynamical behavior of the plasma a variety of instabilities have been observed both remotely and in situ.

A more complex active experiment including both ground-based and sounding rocket experiments with a CRRES chemical release was devised for the El Coqui campaign staged in and over Puerto Rico in 1992. In this experiment the ionosphere was modified by a chemical release from CRRES, then a high power transmitter was used to heat the ionospheric electrons, and the resulting modifications to the ionosphere were monitored in situ by the rocket payloads, and remotely by the Arecibo incoherent scatter radar and optical sensors (Romero and Bernhardt, 1993). This study enabled direct measurements to be made of multi-ion expansion of plasma both parallel and perpendicular to the local geomagnetic field (Szuszczewicz et al., 1993).

Orbital experiments of gas releases were performed during the first Atmospheric Laboratory for Applications and Science (ATLAS-1) mission in 1992 (Torr and Sullivan; 1992; Torr, 1993). Experiments on the CIV effect were made with neutral xenon releases from one of the instruments associated with the Space Experiments and Particle Accelerators (SEPAC) experiment carried on the ATLAS-1 payload (Marshall et al., 1993). In this experiment the xenon was released at a low velocity of 30 m/s relative to the space shuttle, and the fact that the orbital speed of 7.7 km/s exceeds the threshold for critical ionization of 4.2 km/s was used to test the CIV theory. A factor of 60 increase in plasma density was observed by a Langmuir probe mounted in the payload bay supporting the expectation that the released xenon should be partially ionized by the CIV effect. However, there is still some doubt due to the location of the plasma enhancement which modeling showed should have been at least 12 m away from the xenon source, not in the payload bay.

A sounding rocket program of two payloads called CRIT-1 and CRIT-2 (abbreviation of critical ionization), the latter flown in 1989, has been used to look for evidence of critical ionization. Vaporized barium was expelled from the payloads in flight by using a shaped charge which produced a velocity distribution with speeds up to 13 km/sec (Torbert et al., 1992). Particle, wave and ground-based optical measurements during the CRIT-2 flight showed results expected for critical ionization, and this was followed by ionization of the released barium up to yields of 1-2%. Although the CRIT launches were earlier than the reporting period, analysis and interpretation has been reported in the last four years (Stenbaek-Nielsen 1990; Swenson et al., 1990; Kelley et al., 1991, Brenning et al., 1991; Papadopoulos, 1992). While the indications point to an observation of critical ionization, there are still inconsistencies in the data which prevent a definite identification of the phenomenon to be made.

There has been one neutral beam experiment in the reporting period. The Beam Experiments Aboard Rockets (BEAR) sounding rocket experiment was launched from White Sands Missile Range in 1989. The core of this experiment was an accelerator which produced a neutral beam of hydrogen atoms with an energy of 1 MeV and a flux equivalent to a current of 10 mA. The beam was pulsed at 5 Hz, each pulse having a duration of 50 mS. In addition to the accelerator, the payload contained diagnostics to image the beam, monitor the electrical potential of the platform, and determine the characteristics of the emitted beam.



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U.S. National Report to IUGG, 1991-1994
Rev. Geophys. Vol. 33 Suppl., © 1995 American Geophysical Union