While we equip today’s small satellites and in particular CubeSats with progressively sophisticated payloads and let them perform increasingly complex tasks [1], [2], thorough thermal modelling is usually not compatible with development time scales and resources. For a thermal modelling approach to be suitable for small missions, it must mirror their design spirit: It should (a) easily adapt to design modifications, (b) be resource efficient, and (c) be performant enough to allow fast simulations of the whole system. One of the main computational bottlenecks of thermal modelling is the view factor determination to calculate radiative heat transfer [3]. Conventionally, we perform this step using Monte-Carlo Ray Tracing (MCRT) methods. For sm...
For the determination of the solar absorptance αs and ε the thermal emittance optical methods are pr...
We present an algorithm for compressing the radiosity view factor model commonly used in radiation h...
NASA's Edison program is intending to launch a swarm of at least 8 small satellites in 2013. This sw...
The ongoing revolution of space access by means of cost-effective and highly performant small satell...
The ongoing revolution of space access by means of cost-effective and highly performant small satell...
The increasing focus on small satellite missions currently propels space access and will likely serv...
This work is the result of an 8-month cooperation between the author and IDS S.p.A. Company, which i...
In space, satellites are subject to an extreme environment. However, their subsystems are designed t...
One of the main threats for the success of a CubeSat mission is the unbalanced distribution of therm...
There has been an increasing interest in CubeSats missions due to its small size, low cost and flexi...
One of the main threats for the success of a CubeSat mission is the unbalanced distribution of therm...
The aim of this thesis is to design a thermal analysis workflow for design of nano and micro satelli...
In a space mission design, the goal of the thermal control subsystem is to ensure that all component...
This paper addresses the computation of radiative exchange factors through Monte Carlo ray tracing w...
The finite element method (FEM) is widely used in mechanical engineering, especially for space struc...
For the determination of the solar absorptance αs and ε the thermal emittance optical methods are pr...
We present an algorithm for compressing the radiosity view factor model commonly used in radiation h...
NASA's Edison program is intending to launch a swarm of at least 8 small satellites in 2013. This sw...
The ongoing revolution of space access by means of cost-effective and highly performant small satell...
The ongoing revolution of space access by means of cost-effective and highly performant small satell...
The increasing focus on small satellite missions currently propels space access and will likely serv...
This work is the result of an 8-month cooperation between the author and IDS S.p.A. Company, which i...
In space, satellites are subject to an extreme environment. However, their subsystems are designed t...
One of the main threats for the success of a CubeSat mission is the unbalanced distribution of therm...
There has been an increasing interest in CubeSats missions due to its small size, low cost and flexi...
One of the main threats for the success of a CubeSat mission is the unbalanced distribution of therm...
The aim of this thesis is to design a thermal analysis workflow for design of nano and micro satelli...
In a space mission design, the goal of the thermal control subsystem is to ensure that all component...
This paper addresses the computation of radiative exchange factors through Monte Carlo ray tracing w...
The finite element method (FEM) is widely used in mechanical engineering, especially for space struc...
For the determination of the solar absorptance αs and ε the thermal emittance optical methods are pr...
We present an algorithm for compressing the radiosity view factor model commonly used in radiation h...
NASA's Edison program is intending to launch a swarm of at least 8 small satellites in 2013. This sw...