Universitat Politècnica de Catalunya
Universitat Politècnica de Catalunya. e-CAT - Circuits i Transductors Electrònics
2013-05-03
This is a technical report for the early nine test of the first stage of a minilauncher to put up to six femto-satellites in a 250 km Low Earth Orbit. These nine tests were performed in a stone quarry in order to gain experience in real cases to see if student calculations were sized properly. The experiments and simulations were focused in three lines: Determination of the solid propellant burn rate, structural sizing and thermal load.
Preprint
External research report
English
Àrees temàtiques de la UPC::Enginyeria electrònica::Electrònica de potència; Space ships; Mini-Launcher; Solid Propellant; Ammonium Perchlorate Composite Propellant; Astronaus
Technical Report
http://creativecommons.org/licenses/by-nc-nd/3.0/es/
Open Access
Attribution-NonCommercial-NoDerivs 3.0 Spain
E-prints [72991]
