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In-service power requirement for motorised momentum exchange tether in earth-mars mission /Choo Pauline

In-service power requirement for motorised momentum exchange tether in earth-mars mission_Choo Pauline_A2_2014_NI
This project studies on the power requirement for the Motorised Momentum Exchange Tether (MMET) for Earth-Mars mission. From the previous years, interplanetary payload transfer has always been done through conventional rocket propulsion with high costs incurred. Therefore, studies focusing on finding a more economical way for payload transfer with the use of MMET with lower power consumption were carried out. The comparison on the power consumption between both conventional rocket system and the MMET was also conducted alongside with the factors affecting the performance of the MMET .The results were analysed and discussed in detail in this report.
Contributor(s):
Choo Pauline - Author
Language:
English
Subject Keywords:
payload transfer; Motorised Momentum Exchange Tether; rocket
First presented to the public:
6/1/2014
Original Publication Date:
8/7/2019
Previously Published By:
Universiti Sains Malaysia
Place Of Publication:
School of Aerospace Engineering
Citation:
Extents:
Number of Pages - 59
License Grantor / Date Granted:
  / ( View License )
Date Deposited
2019-08-07 16:42:05.751
Submitter:
Nor Hayati Ismail

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In-service power requirement for motorised momentum exchange tether in earth-mars mission /Choo Pauline1 2019-08-07 16:42:05.751
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