東華大學圖書館 |

Language: English

Help

回圖書館首頁

手機版館藏查詢

Back

Switch To: Labeled | MARC Mode | ISBD

Design and Manufacturing of a Single...

Yazicioglu, Ozge,

Linked to FindBook

Google Book

Amazon

博客來

Design and Manufacturing of a Single Langmuir Probe for Plasma Measurements in Hall Effect Thruster Experiments = = Hall Etki̇li̇ Bi̇r Itki̇ Motorunun Plazma Olcumleri̇nde Kullanilmak Uzere Tekli̇ Langmuir Probe Tasarimi ve Ureti̇mi̇ /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Design and Manufacturing of a Single Langmuir Probe for Plasma Measurements in Hall Effect Thruster Experiments =/ Ozge Yazicioglu.
Reminder of title:	Hall Etki̇li̇ Bi̇r Itki̇ Motorunun Plazma Olcumleri̇nde Kullanilmak Uzere Tekli̇ Langmuir Probe Tasarimi ve Ureti̇mi̇ /
Author:	Yazicioglu, Ozge,
Description:	1 electronic resource (96 pages)
Notes:	Source: Masters Abstracts International, Volume: 86-05.
Contained By:	Masters Abstracts International86-05.
Subject:	Chemical bonds. -
Online resource:	https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=31670986
ISBN:	9798342704199

Design and Manufacturing of a Single Langmuir Probe for Plasma Measurements in Hall Effect Thruster Experiments = = Hall Etki̇li̇ Bi̇r Itki̇ Motorunun Plazma Olcumleri̇nde Kullanilmak Uzere Tekli̇ Langmuir Probe Tasarimi ve Ureti̇mi̇ /
Yazicioglu, Ozge,

Design and Manufacturing of a Single Langmuir Probe for Plasma Measurements in Hall Effect Thruster Experiments =Hall Etki̇li̇ Bi̇r Itki̇ Motorunun Plazma Olcumleri̇nde Kullanilmak Uzere Tekli̇ Langmuir Probe Tasarimi ve Ureti̇mi̇ /Ozge Yazicioglu. - 1 electronic resource (96 pages)

Source: Masters Abstracts International, Volume: 86-05.

Electric propulsion is a technology which has been tested on ground and in space since 1960s. The goal of electric propulsion systems is to achieve thrust with high exhaust velocities using electricity. To date, more than 200 electric thrusters have been flown and operated successfully onboard communication satellites and deep-space scientific missions for years with zero failure rate, making the technology more attractive in recent years. Thrust, specific impulse, total efficiency and plume divergence are some figures of merit for the performance of the thruster. Different probes are used in plasma measurements to evaluate and test the performance of the Hall Effect Thrusters. In this study, a Single Langmuir probe design is given for plasma measurements in low pressure. The basic working principle of Single Langmuir probe along with the criteria and measurement methodology applied in the design of the probe is also described. In addition, the technique that is used in the analysis of the current-voltage characteristics to determine the local plasma potential, electron number density and temperature is discussed in detail. Then, the designed probe was produced and used for plasma measurements in low pressure vacuum chamber. The results of measurements and the comparisons with that of Standard ALP System Langmuir Probe are presented in detail.

English

ISBN: 9798342704199Subjects--Topical Terms:

560512
Chemical bonds.

Design and Manufacturing of a Single Langmuir Probe for Plasma Measurements in Hall Effect Thruster Experiments = = Hall Etki̇li̇ Bi̇r Itki̇ Motorunun Plazma Olcumleri̇nde Kullanilmak Uzere Tekli̇ Langmuir Probe Tasarimi ve Ureti̇mi̇ /
LDR:02848nmm a22003973i 4500 001 2433913
005 20250909080246.5
006 m o d
007 cr|nu||||||||
008 261011s2014 miu||||||m |||||||eng d
020 $a 9798342704199
035 $a (MiAaPQD)AAI31670986
035 $a (MiAaPQD)MiddleEastTech24095
035 $a AAI31670986
040 $a MiAaPQD $b eng $c MiAaPQD $e rda
100 1 $a Yazicioglu, Ozge, $e author. $3 3823699
245 1 0 $a Design and Manufacturing of a Single Langmuir Probe for Plasma Measurements in Hall Effect Thruster Experiments = $b Hall Etki̇li̇ Bi̇r Itki̇ Motorunun Plazma Olcumleri̇nde Kullanilmak Uzere Tekli̇ Langmuir Probe Tasarimi ve Ureti̇mi̇ / $c Ozge Yazicioglu.
264 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2014
300 $a 1 electronic resource (96 pages)
336 $a text $b txt $2 rdacontent
337 $a computer $b c $2 rdamedia
338 $a online resource $b cr $2 rdacarrier
500 $a Source: Masters Abstracts International, Volume: 86-05.
500 $a Advisors: Alemdaroglu, Nafiz; Ulusen, Demet.
502 $b M.S. $c Middle East Technical University (Turkey) $d 2014.
520 $a Electric propulsion is a technology which has been tested on ground and in space since 1960s. The goal of electric propulsion systems is to achieve thrust with high exhaust velocities using electricity. To date, more than 200 electric thrusters have been flown and operated successfully onboard communication satellites and deep-space scientific missions for years with zero failure rate, making the technology more attractive in recent years. Thrust, specific impulse, total efficiency and plume divergence are some figures of merit for the performance of the thruster. Different probes are used in plasma measurements to evaluate and test the performance of the Hall Effect Thrusters. In this study, a Single Langmuir probe design is given for plasma measurements in low pressure. The basic working principle of Single Langmuir probe along with the criteria and measurement methodology applied in the design of the probe is also described. In addition, the technique that is used in the analysis of the current-voltage characteristics to determine the local plasma potential, electron number density and temperature is discussed in detail. Then, the designed probe was produced and used for plasma measurements in low pressure vacuum chamber. The results of measurements and the comparisons with that of Standard ALP System Langmuir Probe are presented in detail.
546 $a English
590 $a School code: 2013
650 4 $a Chemical bonds. $3 560512
650 4 $a Energy. $3 876794
650 4 $a Electrons. $3 516581
650 4 $a Charged particles. $3 3682557
650 4 $a Atomic physics. $3 3173870
650 4 $a Chemistry. $3 516420
690 $a 0791
690 $a 0748
690 $a 0485
710 2 $a Middle East Technical University (Turkey). $b Department of Aerospace Engineering. $e degree granting institution. $3 3823700
720 1 $a Alemdaroglu, Nafiz $e degree supervisor.
720 1 $a Ulusen, Demet $e degree supervisor.
773 0 $t Masters Abstracts International $g 86-05.
790 $a 2013
791 $a M.S.
792 $a 2014
856 4 0 $u https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=31670986