Print Email Facebook Twitter CubeSatMicro-Propulsion: Design and Validation of a Micro Bi-Propellant Rocket Motor Title CubeSatMicro-Propulsion: Design and Validation of a Micro Bi-Propellant Rocket Motor Author Powell, S.J. Contributor Cervone, A. (mentor) Faculty Aerospace Engineering Department Space Systems Engineering Programme Space Engineering Date 2015-11-30 Abstract In this MSc thesis, a 4N Bi-Propellant rocket motor was designed using numerical analysis tools. Four motors were built and tested. The results are presented and discussed at length. Combustion instabilities hindered early development. The final design iteration achieved a C* efficiency of greater than 90% in a form factor small enough to fit in a 1U CubeSat module. Subject Micro Bi-Propellant Rocket Motor To reference this document use: http://resolver.tudelft.nl/uuid:a6de0cf0-a562-41e0-8b34-b53b839385d6 Coordinates 52.0167, 4.3667 Part of collection Student theses Document type master thesis Rights (c) 2015 Powell, S.J. Files PDF Thesis_report_V1.4.1_Stef ... _Delft.pdf 23.44 MB Close viewer /islandora/object/uuid:a6de0cf0-a562-41e0-8b34-b53b839385d6/datastream/OBJ/view