Drag deorbit sub-system : (Record no. 175001)

MARC details
000 -LEADER
fixed length control field 04269namaa22004331i 4500
003 - CONTROL NUMBER IDENTIFIER
control field OSt
005 - أخر تعامل مع التسجيلة
control field 20251102112151.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 251019s2024 ua a|||frm||| 000 0 eng d
040 ## - CATALOGING SOURCE
Original cataloguing agency EG-GICUC
Language of cataloging eng
Transcribing agency EG-GICUC
Modifying agency EG-GICUC
Description conventions rda
041 0# - LANGUAGE CODE
Language code of text/sound track or separate title eng
Language code of summary or abstract eng
-- ara
049 ## - Acquisition Source
Acquisition Source Deposit
082 04 - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 629.434
092 ## - LOCALLY ASSIGNED DEWEY CALL NUMBER (OCLC)
Classification number 629.434
Edition number 21
097 ## - Degree
Degree Ph.D
099 ## - LOCAL FREE-TEXT CALL NUMBER (OCLC)
Local Call Number Cai01.13.01.Ph.D.2024.Ah.D
100 0# - MAIN ENTRY--PERSONAL NAME
Authority record control number or standard number Ahmed Aboulftouh Mohamed Ahmed,
Preparation preparation.
245 10 - TITLE STATEMENT
Title Drag deorbit sub-system :
Remainder of title A novel technology for cubesats deorbiting, attitude stabilization and space debris mitigation /
Statement of responsibility, etc. by Ahmed Aboulftouh Mohamed Ahmed ; Supervision Prof. Dr. Mohamed Madbouli Abdelrhman, Prof. Dr. Gamal Mahmoud Sayed El-Bayoumi.
246 15 - VARYING FORM OF TITLE
Title proper/short title نظام المقاومة الفرعي للخروج من المدار :
Remainder of title تقنية حديثة لإزالة الأقمار الصناعية المكعبة من المدار وإستقرار وجهتها وتخفيف الحطام الفضائي /
264 #0 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE
Date of production, publication, distribution, manufacture, or copyright notice 2024.
300 ## - PHYSICAL DESCRIPTION
Extent 131 pages :
Other physical details illustrations ;
Dimensions 30 cm. +
Accompanying material CD.
336 ## - CONTENT TYPE
Content type term text
Source rda content
337 ## - MEDIA TYPE
Media type term Unmediated
Source rdamedia
338 ## - CARRIER TYPE
Carrier type term volume
Source rdacarrier
502 ## - DISSERTATION NOTE
Dissertation note Thesis (Ph.D)-Cairo University, 2024.
504 ## - BIBLIOGRAPHY, ETC. NOTE
Bibliography, etc. note Bibliography: pages 100-106.
520 #3 - SUMMARY, ETC.
Summary, etc. In the first part of this thesis, we used a special perturbation technique as an orbit propagator to model orbital motion and predict the behavior of Cube satellites subjected to perturbations. This technique is a high-precision numerical approach via Cowell's formulation with adaptive step size Runge-Kutta-Fehlberg (RKF78) for numerical integration. The second part of this thesis focuses on the detailed design considerations for implementing a drag deorbit subsystem as a passive attitude actuator. This includes optimizing the geometric characteristics according to stability and lifetime requirements. The effect of the proposed technology on CubeSats attitude stability in different modes of operation is analyzed. Furthermore, numerical simulations are made to assess the performance of the proposed subsystem under different scenarios. The results demonstrate the effectiveness of the drag deorbit subsystem in achieving improved attitude stability and accelerating the decay rate at the end of space mission to mitigate the development of space debris.
520 #3 - SUMMARY, ETC.
Summary, etc. في الجزء الأول من هذه الأطروحة، استخدمنا تقنية اضطراب خاصة كسريان مداري لنمذجة الحركة المدارية والتنبؤ بسلوك الاقمار الصناعية المعرضة للاضطرابات. هذه التقنية هي نهج رقمي عالي الدقة من خلال صياغة Cowell بحجم خطوة متكيف بطريقة RKF78 للتكامل العددي. يركز الجزء الثاني من هذه الأطروحة على اعتبارات التصميم التفصيلية لتنفيذ نظام فرعي لإزالة الأقمار وكمتحكم سلبي للوجهة. يتم تحليل تأثير التكنولوجيا المقترحة على استقرار وجهة القمر في مداره. علاوة على ذلك، يتم إجراء محاكاة رقمية لتقييم أداء النظام الفرعي المقترح في ظل سيناريوهات مختلفة. توضح النتائج فعالية نظام السحب الفرعي في تحقيق استقرار أفضل للموقف واضمحلال المدار في نهاية المهمة الفضائية للحد من تطور الحطام الفضائي.
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Issues CD Issues also as CD.
546 ## - LANGUAGE NOTE
Text Language Text in English and abstract in Arabic & English.
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Artificial satellites
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element الاقمار الصناعية
653 #1 - INDEX TERM--UNCONTROLLED
Uncontrolled term Space debris
-- CubeSats
-- Deorbiting
-- Atmospheric drag
-- Passive Stability
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Mohamed Madbouli Abdelrahman
Relator term thesis advisor.
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Gamal Mahmoud Sayed El-Bayoumi
Relator term thesis advisor.
900 ## - Thesis Information
Grant date 01-01-2024
Supervisory body Mohamed Madbouli Abdelrahman
-- Gamal Mahmoud Sayed El-Bayoumi
Universities Cairo University
Faculties Faculty of Engineering
Department Department of Aerospace Engineering
905 ## - Cataloger and Reviser Names
Cataloger Name Shimaa
Reviser Names Eman Ghareb
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme Dewey Decimal Classification
Koha item type Thesis
Edition 21
Suppress in OPAC No
Holdings
Source of classification or shelving scheme Home library Current library Date acquired Inventory number Full call number Barcode Date last seen Effective from Koha item type
Dewey Decimal Classification المكتبة المركزبة الجديدة - جامعة القاهرة قاعة الرسائل الجامعية - الدور الاول 19.10.2025 92217 Cai01.13.01.Ph.D.2024.Ah.D 01010110092217000 19.10.2025 19.10.2025 Thesis
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