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Mission design and analysis of USM high-altitude balloon / Ahmad Shaqeer Mohamed Thaheer and Norilmi Amilia Ismail

High-altitude balloons (HABs) are unmanned balloons, which are usually filled with helium or hydrogen and can float over approximately 50 km above the sea level. This study aims to develop the mission planner and hardware associated with HAB. The main system of HAB is divided into five subsystems, n...

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Main Authors: Mohamed Thaheer, Ahmad Shaqeer, Ismail, Norilmi Amilia
Format: Article
Language:English
Published: Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM) 2017
Subjects:
Lifting and pressing machinery
Power resources
Energy consumption
Online Access:http://ir.uitm.edu.my/id/eprint/21114/1/AJ_%20Ahmad%20Shaqeer%20Mohamed%20Thaheer%20JME%2017.pdf
http://ir.uitm.edu.my/id/eprint/21114/
https://jmeche.uitm.edu.my/
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spelling my.uitm.ir.211142018-10-23T10:07:47Z http://ir.uitm.edu.my/id/eprint/21114/ Mission design and analysis of USM high-altitude balloon / Ahmad Shaqeer Mohamed Thaheer and Norilmi Amilia Ismail Mohamed Thaheer, Ahmad Shaqeer Ismail, Norilmi Amilia Lifting and pressing machinery Power resources Energy consumption High-altitude balloons (HABs) are unmanned balloons, which are usually filled with helium or hydrogen and can float over approximately 50 km above the sea level. This study aims to develop the mission planner and hardware associated with HAB. The main system of HAB is divided into five subsystems, namely, balloon and navigation, communication, on-board data handling and payload, structure, and thermal system. The design process starts by determining the mission requirements. Through the mission timeline, the flight time is estimated to configure the mode of operation for the mission. A tradeoff analysis is conducted on selected components. The initial selected components that are suitable for the mission are tested individually based on several case studies. After the component testing, the subsystems are integrated and are tested as a whole system. Based on the preliminary results, the configuration and design of the HAB is finalized and a test launch is performed. Finally, the flight test results are collected and analyzed. Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM) 2017 Article PeerReviewed text en http://ir.uitm.edu.my/id/eprint/21114/1/AJ_%20Ahmad%20Shaqeer%20Mohamed%20Thaheer%20JME%2017.pdf Mohamed Thaheer, Ahmad Shaqeer and Ismail, Norilmi Amilia (2017) Mission design and analysis of USM high-altitude balloon / Ahmad Shaqeer Mohamed Thaheer and Norilmi Amilia Ismail. Journal of Mechanical Engineering (JMechE), 14 (2). pp. 62-92. ISSN 1823-5514 ; 2550-164X https://jmeche.uitm.edu.my/
institution Universiti Teknologi Mara
building Tun Abdul Razak Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Mara
content_source UiTM Institutional Repository
url_provider http://ir.uitm.edu.my/
language English
topic Lifting and pressing machinery
Power resources
Energy consumption
spellingShingle Lifting and pressing machinery
Power resources
Energy consumption
Mohamed Thaheer, Ahmad Shaqeer
Ismail, Norilmi Amilia
Mission design and analysis of USM high-altitude balloon / Ahmad Shaqeer Mohamed Thaheer and Norilmi Amilia Ismail
description High-altitude balloons (HABs) are unmanned balloons, which are usually filled with helium or hydrogen and can float over approximately 50 km above the sea level. This study aims to develop the mission planner and hardware associated with HAB. The main system of HAB is divided into five subsystems, namely, balloon and navigation, communication, on-board data handling and payload, structure, and thermal system. The design process starts by determining the mission requirements. Through the mission timeline, the flight time is estimated to configure the mode of operation for the mission. A tradeoff analysis is conducted on selected components. The initial selected components that are suitable for the mission are tested individually based on several case studies. After the component testing, the subsystems are integrated and are tested as a whole system. Based on the preliminary results, the configuration and design of the HAB is finalized and a test launch is performed. Finally, the flight test results are collected and analyzed.
format Article
author Mohamed Thaheer, Ahmad Shaqeer
Ismail, Norilmi Amilia
author_facet Mohamed Thaheer, Ahmad Shaqeer
Ismail, Norilmi Amilia
author_sort Mohamed Thaheer, Ahmad Shaqeer
title Mission design and analysis of USM high-altitude balloon / Ahmad Shaqeer Mohamed Thaheer and Norilmi Amilia Ismail
title_short Mission design and analysis of USM high-altitude balloon / Ahmad Shaqeer Mohamed Thaheer and Norilmi Amilia Ismail
title_full Mission design and analysis of USM high-altitude balloon / Ahmad Shaqeer Mohamed Thaheer and Norilmi Amilia Ismail
title_fullStr Mission design and analysis of USM high-altitude balloon / Ahmad Shaqeer Mohamed Thaheer and Norilmi Amilia Ismail
title_full_unstemmed Mission design and analysis of USM high-altitude balloon / Ahmad Shaqeer Mohamed Thaheer and Norilmi Amilia Ismail
title_sort mission design and analysis of usm high-altitude balloon / ahmad shaqeer mohamed thaheer and norilmi amilia ismail
publisher Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM)
publishDate 2017
url http://ir.uitm.edu.my/id/eprint/21114/1/AJ_%20Ahmad%20Shaqeer%20Mohamed%20Thaheer%20JME%2017.pdf
http://ir.uitm.edu.my/id/eprint/21114/
https://jmeche.uitm.edu.my/
_version_ 1685649423782117376
score 13.250246

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