Numerical simulation of heat pipe thermal performance for aerospace cooling system applications

R Scigliano, V De Simone, R Fusaro, D Ferretto… - Aerospace, 2024‏ - mdpi.com
The design of integrated and highly efficient solutions for thermal management is a key
capability for different aerospace products, ranging from civil aircraft using hydrogen on …

Development and analysis of the thermal design for the OSIRIS-3U CubeSat

MM Garzon - 2012‏ - etda.libraries.psu.edu
Proper spacecraft thermal design ensures spacecraft reliability despite the variations in its
environment that it will encounter, such as heat inputs from the Sun and Earth, and the …

Thermal modelling of a small satellite data processing unit aided by sensitivity analysis and uncertainty quantification

A Jurkowski, R Paluch, M Wójcik, A Klimanek - International Journal of …, 2023‏ - Elsevier
Sensitivity analysis (SA) and uncertainty quantification (UQ) were used to verify the thermal
design of the Intuition-1 nanosatellite data processing unit (DPU). For that purpose, a …

Thermal design procedure for micro-and nanosatellites pointing to earth

T Totani, H Ogawa, R Inoue, TK Das… - … of Thermophysics and …, 2014‏ - arc.aiaa.org
This paper proposes a thermal design procedure for micro-and nanosatellites that can be
completed in one year. Two thermal design concepts keep components within their design …

Water-filled heat pipes for CubeSat thermal control

HJ Van Gerner, H Brouwer, Z De Groot… - IOP Conference Series …, 2021‏ - iopscience.iop.org
Currently, the amount of electrical power that is available for CubeSat's is very small and for
this reason, simple thermal conductance through the frame of the CubeSat is sufficient for …

Performance characterization of water heat pipes and their application in CubeSats

HSB Brouwer - 2016‏ - repository.tudelft.nl
The CubeSat platform has long since its introduction surpassed its original intend of being
an educational and technology demonstration platform only. The recognition and …

[PDF][PDF] Mini Mechanically Pumped Loop Modelling and Design for standardized CubeSat thermal control

J Van Es, T van den Berg, A van Vliet… - 50th International …, 2020‏ - nlr.org
Mini Mechanically Pumped Loop Modelling and Design for standardized CubeSat thermal
control Page 1 50th International Conference on Environmental Systems ICES-2020-294 12-16 …

Mini Mechanically Pumped Loop Modelling, Design and Tests for standardized cubesat thermal control

J van Es, T Ganzeboom, TH van den Berg, A Van Vliet… - 2021‏ - ttu-ir.tdl.org
With the miniaturization of space-borne sensors, more powerful payloads are anticipated to
be used in small satellites. Therefore, new thermal concepts are required to cope with the …

[PDF][PDF] Micro-pumped cooling loop to standardize micro-sat thermal control

J van Esa, A Pauwa, R van den Berga, A van Kleefb - Power, 2018‏ - nlr.org
With the miniaturization of space-borne sensors, more powerful payloads are anticipated to
be used in small satellites. Therefore, new thermal concepts are required to cope with the …

Preliminary thermal design for microsatellites deployed from International Space Station's Kibo Module

DP Mitchao, T Totani, M Wakita, H Nagata - Journal of Thermophysics …, 2018‏ - arc.aiaa.org
A preliminary thermal design was proposed by determining all the possible combinations of
solar absorptivity and infrared emissivity on the panel surfaces of Earth-pointing satellites …