國立虎尾科技大學 |

Satellite Servicing as a Means to Increase Space Mission Resilience in Low Earth Orbit : = A Parametric Architecture Analysis.

紀錄類型:	書目-語言資料,手稿 : Monograph/item
正題名/作者:	Satellite Servicing as a Means to Increase Space Mission Resilience in Low Earth Orbit :/
其他題名:	A Parametric Architecture Analysis.
作者:	Gabriel, Jonathon L.
面頁冊數:	1 online resource (250 pages)
附註:	Source: Masters Abstracts International, Volume: 85-01.
Contained By:	Masters Abstracts International85-01.
標題:	Systems science. -
電子資源:	click for full text (PQDT)
ISBN:	9798379758226

Satellite Servicing as a Means to Increase Space Mission Resilience in Low Earth Orbit : = A Parametric Architecture Analysis.
Gabriel, Jonathon L.

Satellite Servicing as a Means to Increase Space Mission Resilience in Low Earth Orbit :A Parametric Architecture Analysis. - 1 online resource (250 pages)

Source: Masters Abstracts International, Volume: 85-01.

Thesis (M.S.)--University of Maryland, College Park, 2023.

Includes bibliographical references

Satellite servicing and associated capabilities have the potential to establish a new space mission design and operation paradigm throughout Earth orbit. By integrating fundamental elements of the logistics chains that complex engineered systems enjoy on Earth's surface to Earth's orbit, the feasible domain for space missions will significantly expand. Some estimates suggest that the burgeoning satellite servicing industry could generate over 14 billion United States Dollars in revenue over the next decade, driven in large part by growing demand from satellite operators in Low Earth Orbit. However, despite significant economic development and the modern shift of commercial and government space industry focus to Low Earth Orbit, the study of satellite servicing architecture design in this context requires more analysis to mature. Existing satellite servicing mission design literature generally investigates the system design problem as an economic feasibility analysis or system optimization problem. A subpopulation of this literature introduces novel design metrics to the system design process, such as mission flexibility, bringing significant utility to mission designers. In recent years, mission resilience has proven to be a space mission design metric of significant interest to a diverse set of stakeholders such as the United States Department of Defense. Despite its rapidly expanding use, resilience in the context of space mission design has been described primarily qualitatively, limiting its engineering use. Satellite servicing, as with other applications of engineering resilience techniques, aims to integrate capabilities into a complex system that enables a response to system degradation in a favorable manner. This thesis develops a robust simulation framework to parametrically investigate the Low Earth Orbit satellite servicing system design space in the context of scenarios of interest, such as the potentially degrading events of solar storms, orbital debris collisions, and natural satellite failures. A focus will be placed on quantifying the effects on system resilience that satellite servicing can afford Low Earth Orbit constellations. First-order space mission design parameters will be parametrically investigated using the developed analysis and simulation framework. Through leveraging the Earth's J2 perturbation to help route servicer satellites efficiently throughout a constellation of modeled customer satellites, it will be shown that the integration of satellite servicing capabilities into Low Earth Orbit constellations can significantly increase system resilience inside the performance constraints of existing space vehicles. Satellite Servicing system design strategies will be presented that can be employed to increase mission resilience and feasibility.

Electronic reproduction.
Ann Arbor, Mich. :
ProQuest,
2024

Mode of access: World Wide Web

ISBN: 9798379758226Subjects--Topical Terms:

1148479
Systems science.
Subjects--Index Terms:

Low Earth OrbitIndex Terms--Genre/Form:

554714
Electronic books.

Satellite Servicing as a Means to Increase Space Mission Resilience in Low Earth Orbit : = A Parametric Architecture Analysis.
LDR:04220ntm a22003857 4500 001 1149607
005 20241022112555.5
006 m o d
007 cr bn ---uuuuu
008 250605s2023 xx obm 000 0 eng d
020 $a 9798379758226
035 $a (MiAaPQ)AAI30423438
035 $a AAI30423438
040 $a MiAaPQ $b eng $c MiAaPQ $d NTU
100 1 $a Gabriel, Jonathon L. $3 1475911
245 1 0 $a Satellite Servicing as a Means to Increase Space Mission Resilience in Low Earth Orbit : $b A Parametric Architecture Analysis.
264 0 $c 2023
300 $a 1 online resource (250 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: 85-01.
500 $a Advisor: Akin, David L.;Comberiate, Joseph.
502 $a Thesis (M.S.)--University of Maryland, College Park, 2023.
504 $a Includes bibliographical references
520 $a Satellite servicing and associated capabilities have the potential to establish a new space mission design and operation paradigm throughout Earth orbit. By integrating fundamental elements of the logistics chains that complex engineered systems enjoy on Earth's surface to Earth's orbit, the feasible domain for space missions will significantly expand. Some estimates suggest that the burgeoning satellite servicing industry could generate over 14 billion United States Dollars in revenue over the next decade, driven in large part by growing demand from satellite operators in Low Earth Orbit. However, despite significant economic development and the modern shift of commercial and government space industry focus to Low Earth Orbit, the study of satellite servicing architecture design in this context requires more analysis to mature. Existing satellite servicing mission design literature generally investigates the system design problem as an economic feasibility analysis or system optimization problem. A subpopulation of this literature introduces novel design metrics to the system design process, such as mission flexibility, bringing significant utility to mission designers. In recent years, mission resilience has proven to be a space mission design metric of significant interest to a diverse set of stakeholders such as the United States Department of Defense. Despite its rapidly expanding use, resilience in the context of space mission design has been described primarily qualitatively, limiting its engineering use. Satellite servicing, as with other applications of engineering resilience techniques, aims to integrate capabilities into a complex system that enables a response to system degradation in a favorable manner. This thesis develops a robust simulation framework to parametrically investigate the Low Earth Orbit satellite servicing system design space in the context of scenarios of interest, such as the potentially degrading events of solar storms, orbital debris collisions, and natural satellite failures. A focus will be placed on quantifying the effects on system resilience that satellite servicing can afford Low Earth Orbit constellations. First-order space mission design parameters will be parametrically investigated using the developed analysis and simulation framework. Through leveraging the Earth's J2 perturbation to help route servicer satellites efficiently throughout a constellation of modeled customer satellites, it will be shown that the integration of satellite servicing capabilities into Low Earth Orbit constellations can significantly increase system resilience inside the performance constraints of existing space vehicles. Satellite Servicing system design strategies will be presented that can be employed to increase mission resilience and feasibility.
533 $a Electronic reproduction. $b Ann Arbor, Mich. : $c ProQuest, $d 2024
538 $a Mode of access: World Wide Web
650 4 $a Systems science. $3 1148479
650 4 $a Aerospace engineering. $3 686400
653 $a Low Earth Orbit
653 $a Resilience
653 $a Satellite servicing
653 $a System design
653 $a Space vehicles
655 7 $a Electronic books. $2 local $3 554714
690 $a 0538
690 $a 0790
710 2 $a University of Maryland, College Park. $b Aerospace Engineering. $3 1148546
710 2 $a ProQuest Information and Learning Co. $3 1178819
773 0 $t Masters Abstracts International $g 85-01.
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=30423438 $z click for full text (PQDT)