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.
- Title
- Hybrid propulsion system for cubesat applications.
- Creators
- Ozomata D. Ahmed
- Contributors
- Dr. Graham Roberts (Examiner)Prof. Craig Underwood (Examiner)Aaron K. Dr Knoll (Thesis supervisor)University of Surrey (Institution)
- Awarding Institution
- University of Surrey; Doctor of Philosophy (PhD)
- Theses and Dissertations
- Doctor of Philosophy (PhD), University of Surrey
- Number of pages
- 161
- Date submitted
- 18/11/2016
- Grant note
- Funder: Petroleum Technology Development Fund (PTDF), Nigeria
- Identifiers
- 99512777002346
- Copyright
- 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.
- Academic Unit
- School of Computer Science and Electronic Engineering
- Resource Type
- Doctoral Thesis