University of Surrey

Test tubes in the lab Research in the ATI Dance Research

Hybrid propulsion system for cubesat applications.

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

[img]
Preview
Text
PhD_Thesis_AOD.pdf - Version of Record
Available under License Creative Commons Attribution Non-commercial Share Alike.

Download (4MB) | Preview

Abstract

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 :
NameEmailORCID
Ahmed, Ozomata D.ahmedozomata@yahoo.comUNSPECIFIED
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
http://www.loc.gov/loc.terms/relators/THSDr Knoll, Aaron K.a.knoll@surrey.ac.ukUNSPECIFIED
Depositing User : Ozomata Ahmed
Date Deposited : 15 Dec 2016 11:32
Last Modified : 17 May 2017 14:26
URI: http://epubs.surrey.ac.uk/id/eprint/812899

Actions (login required)

View Item View Item

Downloads

Downloads per month over past year


Information about this web site

© The University of Surrey, Guildford, Surrey, GU2 7XH, United Kingdom.
+44 (0)1483 300800