File:Impact of ion propulsion on performance, design, testing and operation of a geosynchronous spacecraft (IA impactofionpropu1094530654).pdf
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Summary[edit]
Impact of ion propulsion on performance, design, testing and operation of a geosynchronous spacecraft ( ) | |
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Author |
Lugtu, Spotrizano Descanzo |
Title |
Impact of ion propulsion on performance, design, testing and operation of a geosynchronous spacecraft |
Publisher |
Monterey, California. Naval Postgraduate School |
Description |
This thesis presents the implementation issues of an ion propulsion subsystem (IPS) on a geosynchronous communications satellite. As an example, Ultra High Frequency (UHF) Follow-On class satellite is selected for this study. The issues include: (1) impact of integration of IPS with other subsystems, such as the electrical power subsystem to take care of the heavy demand of power requirements and location of the subsystem with least impact on attitude control and plume impingement on solar arrays, (2) environmental considerations- particulate contamination, electrostatic discharge (ESD), and electromagnetic interference (EMI), and finally risks and benefits. Ion propulsion offers significant advantages over chemical propulsion due to its high specific impulse and the advent of xenon thruster technology, multikilowatt spacecraft, and nickel-hydrogen (Ni-H2) batteries with demonstrated high cycle life have combined to make the ion thruster attractive for North-South Station Keeping (NSSK). Subjects: Ion rockets; Geostationary satellites.; Ion propulsion; geosynchronous satellite; North-South Station Keeping |
Language | English |
Publication date |
June 1990 publication_date QS:P577,+1990-06-00T00:00:00Z/10 |
Current location |
IA Collections: navalpostgraduateschoollibrary; fedlink |
Accession number |
impactofionpropu1094530654 |
Source | |
Permission (Reusing this file) |
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, may not be copyrighted. |
Licensing[edit]
Public domainPublic domainfalsefalse |
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This file has been identified as being free of known restrictions under copyright law, including all related and neighboring rights. |
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current | 05:26, 9 July 2020 | 1,275 × 1,650, 177 pages (5.12 MB) | Fæ (talk | contribs) | FEDLINK - United States Federal Collection impactofionpropu1094530654 (User talk:Fæ/IA books#Fork8) (batch 1990-1992 #4956) |
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Short title | Impact of ion propulsion on performance, design, testing and operation of a geosynchronous spacecraft |
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Author | Lugtu, Spotrizano Descanzo |
Software used | Lugtu, Spotrizano Descanzo |
Conversion program | |
Encrypted | no |
Page size |
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Version of PDF format | 1.4 |