Trajectory design for alibration point mission / Rasha Mohamed Fathy Ghoneim ; Supervised Mervat Elsayed Awad , Moustafa Kamal Mahmoud , Gerard Gomez

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Rasha Mohamed Fathy Ghoneim

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Material type: Text

TextLanguage: eng Publication details: Cairo : Rasha Mohamed Fathy Ghoneim , 2009Description: 108Leaves : charts ; 30cmOther title:

تصميم مسار رحلة لنقاط النودان [Added title page title]

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Dissertation note: Thesis (Ph.D.) - Cairo University - Faculty of Science - Department of Astronomy and Meteorology Summary: The interest in missions utilizing trajectories near the Lagrangian libration points has been recently noticeably increased . The present work aims at exploring the aspects and solutions of the restricted three body problem that are relevant to the dynamics and mission analysis of orbits about the libration points .

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Holdings
Item type	Current library	Home library	Call number	Copy number	Status	Date due	Barcode
Thesis	قاعة الرسائل الجامعية - الدور الاول	المكتبة المركزبة الجديدة - جامعة القاهرة	Cai01.12.01.Ph.D.2009.Ra.T (Browse shelf(Opens below))		Not for loan		01010110052304000
CD - Rom	مخـــزن الرســائل الجـــامعية - البدروم	المكتبة المركزبة الجديدة - جامعة القاهرة	Cai01.12.01.Ph.D.2009.Ra.T (Browse shelf(Opens below))	52304.CD	Not for loan		01020110052304000

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Previous	Cai01.12.01.Ph.D.2009.Na.E Effect of an artificial radiant force on the spaceceraft's orbit /	Cai01.12.01.Ph.D.2009.Na.E Effect of an artificial radiant force on the spaceceraft's orbit /	Cai01.12.01.Ph.D.2009.Ra.T Trajectory design for alibration point mission /	Cai01.12.01.Ph.D.2009.Ra.T Trajectory design for alibration point mission /	Cai01.12.01.Ph.D.2009.Su.S Space environment and its effect on spacecrafts /	Cai01.12.01.Ph.D.2009.Su.S Space environment and its effect on spacecrafts /	Cai01.12.01.Ph.D.2009.Wa.C Coorbital motion with the earth as a central body /	Next

Thesis (Ph.D.) - Cairo University - Faculty of Science - Department of Astronomy and Meteorology

The interest in missions utilizing trajectories near the Lagrangian libration points has been recently noticeably increased . The present work aims at exploring the aspects and solutions of the restricted three body problem that are relevant to the dynamics and mission analysis of orbits about the libration points .

Issued also as CD

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