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Hybrid propulsion system for cubesat applications.

Ahmed, Ozomata D. (2016) Hybrid propulsion system for cubesat applications. Doctoral thesis, University of Surrey.

PhD_Thesis_AOD.pdf - Version of Record
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The CubeSats platform has become a common basis for the development and flight of very small, low cost spacecraft-particularly amongst University groups. The smallest CubeSats are just 1 litre in volume-comprising a 10.

Item Type: Thesis (Doctoral)
Subjects : Satellite Propulsion Systems
Divisions : Theses
Authors :
Ahmed, Ozomata
Date : 30 November 2016
Funders : Petroleum Technology Development Fund (PTDF), Nigeria
Copyright Disclaimer : This thesis is from my research for the award of PhD from University of Surrey. Any material used in the thesis, maybe partially, in full, as picture or table is duly acknowledged and referenced in the thesis. This work has not been submitted anywhere for any award. It is an original work of Ahmed Ozomata David.
Contributors :
ContributionNameEmailORCID Knoll, Aaron
Depositing User : Ozomata Ahmed
Date Deposited : 15 Dec 2016 11:32
Last Modified : 31 Oct 2017 18:57

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