Browsing by Subject "Microspacecraft"
Now showing items 1-12 of 12
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Bus d'un microstaèl·lit en òrbita de la Terra
(Universitat Politècnica de Catalunya, 2006-12-20)
Master thesis (pre-Bologna period)
Open AccessEn aquest treball es pretén realitzar el disseny basic, o disseny de fase A, d’un microsatèl•lit per a una missió en orbita al voltant de la Terra. L’objectiu d’aquesta missió es mesurar els efectes de la radiació ionitzant ... -
Design and Implementation of a femto-satellite technology demonstrator
(Universitat Politècnica de Catalunya, 2011-07-05)
Master thesis
Open AccessThe present work is aimed to demonstrate the development and implementation of a scalable femto-satellite technology demonstrator, experimentation and development platform in order to practically prove the possibility ... -
Implementation of a femto-satellite and a mini-launcher for the N Prize
(Universitat Politècnica de Catalunya, 2010-05-20)
Master thesis
Open AccessIn this Master Thesis we begin with a short analysis of the current space market, with the aim of searching solutions that allow us to implement femto-satellites (that is, satellites with a mass less than 100 grams) and ... -
Mission and Thermal Analysis of UPC Cubesat
(Universitat Politècnica de Catalunya, 2009-12-22)
Master thesis
Open Access -
Optimització i desenvolupament de l'estructura mecànica de l'ordinador a bord del cubesat C3SatP
(Universitat Politècnica de Catalunya, 2019-07-12)
Bachelor thesis
Restricted access - author's decisionThe main challenge of space missions is based on finding new formulas to make space more accessible. The main limiting factors are related with high cost of the missions and the weight of the elements. For this reason, the ... -
Power efficiency enhancement of transmitters using adaptive envelope tracking and shaping techniques for small payload space applications
(Universitat Politècnica de Catalunya, 2015-09-28)
Master thesis
Open AccessWith the rise of modular system architecture for distributed satellite systems with multiple small payloads instead of conventional larger spacecrafts, the efficient characterization of power budget and available ... -
Structural analysis of a CubeSat
(Universitat Politècnica de Catalunya, 2020-07-14)
Bachelor thesis
Restricted access - author's decisionThis Treball Final de Grau consists on developing, executing and assessing the results of a series of FEM structural analyses aimed to demonstrate the that the 3CAT-4 nanosatellite complies with all necessary structural ... -
Study of a low cost inertial platfom for a femto-satellite deployed by a mini-launcher
(Universitat Politècnica de Catalunya, 2010-07-28)
Bachelor thesis
Open Access -
Study of a nozzle vector control for a low cost mini-launcher
(Universitat Politècnica de Catalunya, 2011-07-07)
Master thesis
Open AccessThis study is addressed to the control system of a mini-launcher. A reaction control based on purge pressure from a solid propellant engine of a main stage, or using cold gas from a storage tank will be the control method. ... -
Study of space condition effect and analyzing digital techniques for improving RF power amplifier's linearity and efficiency for small satellites
(Universitat Politècnica de Catalunya, 2015-09-28)
Master thesis
Open AccessObjective of modern small satellite communication is to provide the end users with higher data rate downlink capability, in addition to, reliability and system efficiency. A significant device, with respect to power ... -
Thermal analysis and testing for CubeSat based missions
(Universitat Politècnica de Catalunya, 2021-07-23)
Bachelor thesis
Restricted access - author's decisionThe boom of the New Space sector has been mainly influenced by one concept: the CubeSat standard. The use of this standard has increased the COTS products utilization. Therefore, the components¿ testing has become paramount ... -
Use of hardware-on-the-loop to test missions for a low cost mini-launcher
(Universitat Politècnica de Catalunya, 2011-02-28)
Bachelor thesis
Open AccessEste estudio esta dirigido al uso de lazos de control por Hardware para probar subsistemas tanto de femto-satelites como mini-lanzaderas. Usaremos el simulador Moon2.0 para implementar comunicaciones entre una caja negra ...
