In this thesis the main components of a propulsion system for CubeSats and their integration have been analysed. First of all, a brief description of what a CubeSat is, and its main application have been described and after that the state of the art of different propulsion mechanisms has been explained. In the second part of the thesis the architecture of the hydrogen peroxide propulsion has been described and the most important components have been found among the ones available on the market. In the end, a 3D render has been realized in order to explain the chosen architecture, with a particular focus on the tank which has been designed specifically for this application, because any useful tank has been found on the market
The purpose of this Thesis is to develop the design process of the pressurised propellant tank for a...
In the past decade, CubeSats have revolutionized small spacecraft missions. These miniature satellit...
The format and size specifications of the CubeSat platform require highly miniaturized subsystems, o...
As CubeSats prove their ability to capture images and collect data, space operators plan to send the...
At the moment, it does not exist a low-cost propulsion system in the market capable of providing thr...
Nowadays, the demand of providing CubeSats for a propulsion system is increasing parallel to their g...
The trend of recent years shows a growing interest in small satellites. In particular, a platform th...
Cubesats and other nano- and pico-satellite platforms have traditionally not had the capability of o...
Universities and agencies, such as NASA, are looking to utilize CubeSats as a low-cost tool for scie...
CubeSats provide a cost effective means to perform scientific and technological studies in space. Du...
The present thesis is concerned with the realization and preliminary tests verification of an innova...
Stellar Exploration Inc. has developed a high performance Hydrazine Monopropellant Micro Propulsion ...
Cold gas propulsion systems offer today’s CubeSats a relatively simple propulsion solution, but with...
This project presents the design, fabrication, and testing of a flight-like hydrogen peroxide ...
Interplanetary CubeSat missions enable low-cost exploration missions, in which the design of a prima...
The purpose of this Thesis is to develop the design process of the pressurised propellant tank for a...
In the past decade, CubeSats have revolutionized small spacecraft missions. These miniature satellit...
The format and size specifications of the CubeSat platform require highly miniaturized subsystems, o...
As CubeSats prove their ability to capture images and collect data, space operators plan to send the...
At the moment, it does not exist a low-cost propulsion system in the market capable of providing thr...
Nowadays, the demand of providing CubeSats for a propulsion system is increasing parallel to their g...
The trend of recent years shows a growing interest in small satellites. In particular, a platform th...
Cubesats and other nano- and pico-satellite platforms have traditionally not had the capability of o...
Universities and agencies, such as NASA, are looking to utilize CubeSats as a low-cost tool for scie...
CubeSats provide a cost effective means to perform scientific and technological studies in space. Du...
The present thesis is concerned with the realization and preliminary tests verification of an innova...
Stellar Exploration Inc. has developed a high performance Hydrazine Monopropellant Micro Propulsion ...
Cold gas propulsion systems offer today’s CubeSats a relatively simple propulsion solution, but with...
This project presents the design, fabrication, and testing of a flight-like hydrogen peroxide ...
Interplanetary CubeSat missions enable low-cost exploration missions, in which the design of a prima...
The purpose of this Thesis is to develop the design process of the pressurised propellant tank for a...
In the past decade, CubeSats have revolutionized small spacecraft missions. These miniature satellit...
The format and size specifications of the CubeSat platform require highly miniaturized subsystems, o...