000826686 000__ 03352cam\a2200457Ii\4500 000826686 001__ 826686 000826686 005__ 20230306144415.0 000826686 006__ m\\\\\o\\d\\\\\\\\ 000826686 007__ cr\cn\nnnunnun 000826686 008__ 180305s2018\\\\gw\a\\\\ob\\\\000\0\eng\d 000826686 019__ $$a1028609719$$a1028651115$$a1028815063$$a1028899918$$a1028945034$$a1028969015$$a1029003272$$a1029207296$$a1029237055$$a1029323957 000826686 020__ $$a9783658212094$$q(electronic book) 000826686 020__ $$a3658212098$$q(electronic book) 000826686 020__ $$z9783658212087 000826686 020__ $$z365821208X 000826686 0247_ $$a10.1007/978-3-658-21209-4$$2doi 000826686 035__ $$aSP(OCoLC)on1027221505 000826686 035__ $$aSP(OCoLC)1027221505$$z(OCoLC)1028609719$$z(OCoLC)1028651115$$z(OCoLC)1028815063$$z(OCoLC)1028899918$$z(OCoLC)1028945034$$z(OCoLC)1028969015$$z(OCoLC)1029003272$$z(OCoLC)1029207296$$z(OCoLC)1029237055$$z(OCoLC)1029323957 000826686 040__ $$aGW5XE$$beng$$erda$$epn$$cGW5XE$$dN$T$$dYDX$$dOCLCF$$dEBLCP$$dMERER 000826686 049__ $$aISEA 000826686 050_4 $$aTL782 000826686 08204 $$a629.134/354$$223 000826686 1001_ $$aHey, Franz Georg,$$eauthor. 000826686 24510 $$aMicro Newton thruster development :$$bdirect thrust measurements and thruster downscaling /$$cFranz Georg Hey. 000826686 264_1 $$aWiesbaden, Germany :$$bSpringer Vieweg,$$c2018. 000826686 300__ $$a1 online resource (xvii, 171 pages) :$$billustrations 000826686 336__ $$atext$$btxt$$2rdacontent 000826686 337__ $$acomputer$$bc$$2rdamedia 000826686 338__ $$aonline resource$$bcr$$2rdacarrier 000826686 504__ $$aIncludes bibliographical references. 000826686 5050_ $$aIntro; Acknowledgements; Contents; List of Figures; List of Tables; List of Acronyms; 1 Introduction; 1.1 Missions for Micro-Newton Thruster Applications; 1.2 Micro Propulsion Thrusters Overview; 1.3 Micro Newton Test Facilities in Europe; 1.4 Airbus Development Approach; 2 Electric Propulsion Fundamentals; 2.1 Basic Equations; 2.2 Basic Plasma Physics; 2.3 Electric Propulsion Thruster Types; 2.3.1 Field Emission Electric Propulsion; 2.3.2 Radio Frequency Ion Thruster; 2.3.3 High Efficiency Multistage Plasma Thruster; 2.4 Thruster Characterisation; 2.4.1 Direct Thrust Measurement 000826686 5058_ $$a2.4.2 Indirect Thrust Measurement3 Micro-Newton Thruster Test Facility; 3.1 Vacuum Facility; 3.2 Plasma Diagnostic Setup; 3.2.1 Faraday Cup; 3.2.2 Retarding Potential Analyser; 3.2.3 Plasma Diagnostic Calibration; 3.3 Airbus Micro-Newton Thrust Balance; 3.3.1 Mechanical Balance Setup; 3.3.2 Optical Balance Readout; 3.3.3 Thrust Balance Controlling and Data Acquisition; 3.3.4 Balance Calibration and Uncertainty Analysis; 3.3.5 Thrust Balance Characterisation, Testing and Analysis; 3.4 Test Facility Real Thruster Measurement Results and Analysis 000826686 5058_ $$a4 Micro High Efficiency Multistage Plasma Thruster Development4.1 Next Generation µHEMPT Development Approach; 4.2 The Next Generation µHEMPT; 4.2.1 Full Size NG-µHEMPT; 4.2.2 Miniaturised NG-µHEMPT; 4.3 NG-µHEMPT Development Summary; 5 Conclusion and Outlook; Bibliography; Appendix 000826686 506__ $$aAccess limited to authorized users. 000826686 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed March 5, 2018). 000826686 650_0 $$aRocket engines$$xThrust. 000826686 77608 $$iPrint version: $$z365821208X$$z9783658212087$$w(OCoLC)1022781050 000826686 852__ $$bebk 000826686 85640 $$3SpringerLink$$uhttps://univsouthin.idm.oclc.org/login?url=http://link.springer.com/10.1007/978-3-658-21209-4$$zOnline Access$$91397441.1 000826686 909CO $$ooai:library.usi.edu:826686$$pGLOBAL_SET 000826686 980__ $$aEBOOK 000826686 980__ $$aBIB 000826686 982__ $$aEbook 000826686 983__ $$aOnline 000826686 994__ $$a92$$bISE