EVALUATION OF MAGNESIUM AS A HALL THRUSTER PROPELLANT

In this study, the use of magnesium as a Hall thruster propellant was evaluated. A xenon Hall thruster was modified such that magnesium propellant could be loaded into the anode and use waste heat from the thruster discharge to drive the propellant vaporization. A control scheme was developed, which allowed for precise control of the mass flow rate while still using plasma heating as the main mechanism for evaporation. The thruster anode, which also served as the propellant reservoir, was designed such that the open area was too low for sufficient vapor flow at normal operating temperatures (i.e. plasma heating alone). The remaining heat needed to achieve enough vapor flow to sustain thruster discharge came from a counter-wound resistive heater located behind the anode. The control system has the ability to arrest thermal runaway in a direct evaporation feed system and stabilize the discharge current during voltage-limited operation. A proportional-integral-derivative control algorithm was implemented to enable automated operation of the mass flow control system using the discharge current as the measured variable and the anode heater current as the controlled parameter. Steady-state operation at constant voltage with discharge current excursions less than 0.35 A was demonstrated for 70 min. Using this long-duration method, stable operation was achieved with heater powers as low as 6% of the total discharge power. Using the thermal mass flow control system the thruster operated stably enough and long enough that performance measurements could be obtained and compared to the performance of the thruster using xenon propellant. It was found that when operated with magnesium, the thruster has thrust ranging from 34 mN at 200 V to 39 mN at 300 V with 1.7 mg/s of propellant. It was found to have 27 mN of thrust at 300 V using 1.0 mg/s of propellant. The thrust-to-power ratio ranged from 24 mN/kW at 200 V to 18 mN/kW at 300 volts. The specific impulse was 2000 s at 200 V and upwards of 2700 s at 300 V. The anode efficiency was found to be ~23% using magnesium, which is substantially lower than the 40% anode efficiency of xenon at approximately equivalent molar flow rates. Measurements in the plasma plume of the thruster—operated using magnesium and xenon propellants—were obtained using a Faraday probe to measure off-axis current distribution, a retarding potential analyzer to measure ion energy, and a double Langmuir probe to measure plasma density, electron temperature, and plasma potential. Additionally, the off axis current distributions and ion energy distributions were compared to measurements made in krypton and bismuth plasmas obtained in previous studies of the same thruster. Comparisons showed that magnesium had the largest beam divergence of the four propellants while the others had similar divergence. The comparisons also showed that magnesium and krypton both had very low voltage utilization compared to xenon and bismuth. It is likely that the differences in plume structure are due to the atomic differences between the propellants; the ionization mean free path goes down with increasing atomic mass. Magnesium and krypton have long ionization mean free paths and therefore require physically larger thruster dimensions for efficient thruster operation and would benefit from magnetic shielding.

Sink mat for broken glass plate negative

Broken glass plate negative. Goal To design a simple protective enclosure for the two pieces of the glass plate negative, that allows the user to visualize the image as a whole. Treatment A sink mat was created by layering museum board and Volera foam, and "sinks" cut to fit the broken pieces along with thumb notches for ease of lifting. A portfolio of e-flute board, buckram, and cotton ties was built up around the sink mat to provide a protective enclosure that is easily stored on edge.

Fiel relazion de los terremotos, que siguiuiren en esta ciudad de Liorna en nel mes de henero de este anno 1740 ...

[von] Abraham de Bargas

Sēfer talmîd ṣaḥqān mûsārî : ... ḥibbûr qāṭān ... mē-haw-wikkûaḥ še-hāyā bên 2 talmîdîm ôhāvîm we-rāʿîm mē-ḥāmat haṣ-ṣāḥôq ... ʿim marʿê māqôm mit-Tôrā nevîʿîm û-Ktûvîm û-min-hat-Talmûd... der gilernṭi und bikerṭi špilr ...

[Jehuda Arje aus Modena]

Les Antilles et la représentation de l'espace transatlantique chez Maryse Condé

Si Maryse Condé, écrivain française originaire de la Guadeloupe, semble s’être sentie chez elle dans l’ensemble du monde atlantique (elle a résidé aux Antilles, en France, aux Etats-Unis, en Afrique), ainsi certaines de ses œuvres, alors même qu’elles prennent pour cadre de référence les Antilles, témoignent d’une rare capacité à s’approprier tout l’espace atlantique, que ce soit à travers les mouvements réels, libres ou forcés, des protagonistes ou au contraire par le biais de leurs souvenirs et rêveries. L’analyse des Derniers rois mages (1992), en particulier, nous permettra de dégager l’originalité de Maryse Condé en ce qui concerne la représentation de cet espace – espace non plus organisé en fonction des cartographies imaginaires figées fournies par l’impérialisme, la « négritude » ou la « créolité », mais traversé par une dynamique exploratoire, multifocale et non fusionnelle.

Studien aus Toynbee-Hall

S.

Bilder aus Toynbee-Hall

S.

Bilder aus Toynbee-Hall : III.

S.