EXPERIMENTS ON CHARGE AND MOMENTUM EXCHANGE BETWEEN IONS AND MOLECULES IN THE DEVELOPMENT OF HIGH-SPEED MOLECULAR BEAMS
Charge and momentum exchange between ions and molecules in developing high speed molecular beams
MOLECULAR BEAM↗
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Computer experiments with charged particles, charged fluids and plasmas - A classification and bibliography
Computer methods for solving many-body and charged particle problems and nonlinear systems, classification and bibliography
CHARGED PARTICLE↗
Charge deflection experiments in beam foil spectroscopy.
Static beam deflection in beam foil spectroscopy for determining parent ionization stage of emitting ions
Fink, U.↗
An energetic charged particle experiment on the asteroid/Jupiter missions, Pioneers F andG
The experiment package, consisting of seven Geiger-Mueller tubes as basic sensors, is described, including the instrumental characteristics and tube arrangements. The capabilities of surveying the absolute intensities, energy spectra, angular distributions of energetic electrons and protons in the Jupiter magnetosphere are discussed.
Vanallen, J. A.↗
Nuclear radiation interference and damage effects in charged particle experiments for extended space missions.
Demonstration that meaningful galactic and solar cosmic radiation measurements can be carried out on deep space missions. The radioisotopic thermoelectric generators (RTGs) which must be used as a source of power and perhaps of heat are a problem, but with proper separation from the experiments, with orientation, and with some shielding the damage effects can be reduced to an acceptable level. The Pioneer spacecraft are crucial in that they are targeted at the heart of Jupiter's radiation belts, and should supply the details of those belts. The subsequent Grand Tour opportunities can be selected for those periods which result in larger distances of closest approach to Jupiter if necessary.
Trainor, J. H.↗
Jupiter revisited - First results from the University of Chicago charged particle experiment on Pioneer 11
The data obtained by Pioneer 11 confirmed results from Pioneer 10 and provided new information for an understanding of the physics of the Jovian magnetosphere. Attention is given to the significance of Pioneer 11 data in relation to two fundamentally different models which have been proposed to account for the variations in the electron flux observed in Jupiter's outer magnetosphere. Proton flux characteristics are considered, taking into account the intensity profiles of energetic particles trapped in the dipole region of Jupiter's magnetic field.
Simpson, J. A.↗
The L equals 6.7 quiet time barium shaped charge injection experiment 'Chachalaca'
Near dawn on October 9, 1972, UT, a barium plasma injection experiment was carried out from Poker Flat, Alaska, during quiet magnetic conditions (Kp equals 1+). The visible plasma flux tube produced was more diffuse than the flux tubes in previous experiments, but it could be tracked for 30 min out to an altitude of 2.5 earth radii. The flux tube remained integral for about 20 min, when a single striation separated from the main streak. Comparisons of the observed flux tube orientation with theoretical field models show no significant deviations ascribable to field-aligned currents. Cross-field drift rates of the foot of the flux tube indicate an E field of approximately 7 mV/m at 200-km altitude. Although an attempt was made via a jet aircraft flight, barium ions were not detected in the southern conjugate region. No energetic particle precipitation phenomena were observed which could be ascribed to the barium plasma injection.
Wescott, E. M.↗
Nuclear and ionic charge distribution experiment on ISEE-1 and ISEE-3
The experimental work carried out under this contract is a continuation of that originally performed under Contracts NAS5-20062 and NAS5-26739. The data analyzed are from the Max-Planck Institut/Univ. of Maryland experiment on ISEE-1 and ISEE-3. Each spacecraft experiment consists of a nearly identical set of three sensors (designated the ULECA, ULEWAT, and ULEZEQ sensors) designed to measure the energy spectra and composition of suprathermal and energetic ions over a broad energy range (less than 3 keV/e to more than 20 MeV/nucleon). Since the launch of ISEE's 2 and 3, the MPI/Univ. of Maryland experiments have generally performed as expected except for a partial failure of the ULEWAT sensor on ISEE-1 in August 1978. A number of scientific studies have either been completed, initiated or are at various stages of completion. A brief summary of Primary Results is given, followed by a more detailed summary of the major accomplishments at the Univ. of Maryland.
Gloeckler, G.↗
Signal Conditioning for Satellite Borne Energetic-Charged-Particle Experiments
Many of the spacecraft launched thus far have carried detectors for investigating cosmic rays, solar protons, solar plasmas, and the geomagnetically trapped radiation. These detectors, which will find continued application in the future, include ion chambers; proportional, Geiger-Muller, scintillation, Cerenkov, and solid state detectors; ion collectors; and nuclear emulsions. The instrumentation required to condition the signals from these detectors prior to telemetering is steadily growing more complex in order to permit more meaningful measurements. This report describes a number of instrumentation elements typical of the present state of the art, and a present-generation three-detector system which illustrates the integration of such basic elements into a complex system.
Ludwig, George H.↗
Characterizing the Performance of the Wheel Electrostatic Spectrometer
Insulators need to be discharged after each wheel revolution. Sensor responses repeatable within one standard deviation in the noise of the signal. Insulators may not need to be cleaned after each revolution. Parent Technology- Mars Environmental Compatibility Assessment/Electrometer Electrostatic sensors with dissimilar cover insulators Protruding insulators tribocharge against regolith simulant Developed for use on the scoop for the 2001 Mars Odyssey lander Wheel Electrostatic Spectrometer Embedded electrostatic sensors in prototype Martian rover wheel If successful, this technology will enable constant electrostatic testing on Mars Air ionizing fan used to neutralize the surface charge on cover insulators . WES rolled on JSClA lunar simulant Control experiment -Static elimination not conducted between trials -Capacitor discharged after each experiment Charge neutralization experiment -Static elimination conducted between trials -Capacitor discharged after each experiment. Air ionizing fan used on insulators after each wheel revolution Capacitor discharged after each trial Care was taken to roll WES with same speed/pressure Error bars represent one standard deviation in the noise of e ach sensor
Johansen, Michael R.↗
Experiments On Rotating, Charged Liquid Drops
Report describes experiments in which electrically charged drops of liquid levitated electrostatically and rotated and vibrated acoustically. Discusses possibility of measuring charges of drops of low-viscosity liquids by drop-oscillation method, and measurement of surface tensions of highly viscous liquids by drop-rotation method. Results have implications for containerless processing and modeling of atomic nuclei.
Rhim, Won-Kyu↗
Plasma-depleted holes, waves, and energized particles from high-altitude explosive plasma perturbation experiments
The results of high-explosive shaped charge experiments King Crab and Bubble Machines I and II, intended to perturb the ambient plasma and magnetic field, are discussed. The instrumentation was flown above an altitude of 460 km in March 1980 and 1981 and comprised a single-axis dipole electric field detector, a fixed bias cylindrical Langmuir probe, a three-axis attitude magnetometer, and curved plated energetic ion and electron electrostatic analyzer. Among the effects of the explosion which are detailed, emphasis is placed on the creation of an ion-depleted dark hole during the Bubble Machine II experiment; mechanisms explaining the phenomenon are outlined. The auroral intensity ion beams with energies of up to 6.8 keV, observed following the explosion in the field-aligned ion electrostatic analyzer, are suggested to represent an existing ion conic population pitch angle scattered by the released barium into the view of the detector.
Wescott, E. M.↗
NASCAP/LEO simulations of Shuttle Orbiter charging during the SAMPIE experiment
The electrostatic charging of the Space Shuttle Orbiter during the operation of the Solar Array Module Plasma Interaction Experiment (SAMPIE) was modeled using the NASA Charging Analyzer Program/ low Earth orbit (NASCAP/LEO) computer code. The SAMPIE experiment consists of an array of various solar cells representing the present technologies. The objectives of the experiment are to investigate the arcing and current collection characteristics of these cells when biased to high potentials in a LEO plasma. NASCAP/LEO is a 3-D code designed to simulate the electrostatic charging of a spacecraft exposed to a plasma at LEO or ground test conditions. At its most extreme configuration, with the largest array segment of the SAMPIE experiment biased + 600 V with respect to the orbiter and facing the ram direction, the computer simulations predict that the orbiter's potential will be approximately -20 V with respect to the plasma.
Chock, Ricaurte↗
A method for non-contact drop charge measurement
A new approach for detecting point type of charge has been developed. This system is based on the principle of reciprocal motion of a grounded conductor near a point charge. The current induced through such a process can then be used to determine the static field strength of the point charge, hence the quantity of the charge. Experiments were done to understand the characteristics of this new device. Test case indicates that the results are in good agreement with the theoretical prediction. This device shows extremely good linearity with respect to the strength of the input static field. The resolution of the system is better than 10 V/m, which is about two orders of magnitude in sensitivity higher than other types of field measuring apparatus. The high sensitivity of this system makes it possible to conduct charged drop experiments under microgravity conditions.
Lin, K. C.↗
Explosive plasma releases in the earth's ionosphere
The Trigger and Buaro experiments and the University of Alaska's radial shaped charge experiment, which were conducted to actively probe the ionosphere with expanding plasmas are described. Emphasis is on the Trigger experiment, which has a Cs release with spherical geometry. Transient events occurring after Cs detonation include the production of a 200 mV/m electric field pulse, and the precipitation of energetic electrons. Future applications are also discussed, and include in situ measurements of the radial shaped experiment from a mother-daughter payload.
Kintner, P. M.↗
Experiments on regulation of electric charge on space vehicles
Spacecraft at geosynchronous altitudes have been observed to charge to potentials of many kilovolts. Anomalous behavior of spacecraft systems are believed to have resulted from discharges associated with these charging events. Experiments in modifying spacecraft charge have been conducted with ion and electron emitters on the ATS-5, ATS-6 and SCATHA spacecraft. The experiments have been successful in discharging highly charged spacecraft, in reducing the amount of differential charging on spacecraft surfaces, and in inducing charging on otherwise uncharged or nominally charged spacecraft. Regulation of vehicle charge allows better measurements of the plasma environment and should reduce anomalous spacecraft behavior.
Whipple, E. C., Jr.↗
Discrete Element Modeling (DEM) of Triboelectrically Charged Particles: Revised Experiments
In a previous work, the addition of basic screened Coulombic electrostatic forces to an existing commercial discrete element modeling (DEM) software was reported. Triboelectric experiments were performed to charge glass spheres rolling on inclined planes of various materials. Charge generation constants and the Q/m ratios for the test materials were calculated from the experimental data and compared to the simulation output of the DEM software. In this paper, we will discuss new values of the charge generation constants calculated from improved experimental procedures and data. Also, planned work to include dielectrophoretic, Van der Waals forces, and advanced mechanical forces into the software will be discussed.
Hogue, Michael D.↗
Active experiments in space in conjunction with Skylab
Two papers are presented which relate to the Skylab barium shaped charge experiments. The first describes the L=6.6 OOSIK barium plasma injection experiment and magnetic storm of March 7, 1972. Rocket payload, instrumentation, data reduction methods, geophysical environment at the time of the experiment, and results are given. The second paper presents the observation of an auroral Birkeland current which developed from the distortion of a barium plasma jet during the above experiment.
Wescott, E. M.↗