On‐Orbit Thermal Design and Validation of 1 U Standardized CubeSat of STEP Cube Lab

SJ Kang, HU Oh - International Journal of Aerospace …, 2016 - Wiley Online Library
The Cube Laboratory for Space Technology Experimental Projects (STEP Cube Lab) is a
cube satellite (CubeSat) classified as a pico‐class satellite of 1 U (unit) size. Its main mission …

Analytical investigation of a nanosatellite panel surface temperatures for different altitudes and panel combinations

M Bulut, N Sozbir - Applied Thermal Engineering, 2015 - Elsevier
The thermal control of future nanosatellite will be challenging due to dedicated panel
surface area for radiation. The thermal control concept is to keep the payload within …

Thermal design, analysis, and testing of the first Turkish 3U communication CubeSat in low earth orbit

M Bulut - Journal of Thermal Analysis and Calorimetry, 2021 - Springer
TURKSAT-3USAT is the first Turkish communication 3U CubeSat designed and built by the
students of the Space Systems Design and Test Laboratory and Radio Frequency …

Thermal modeling of CIIIASat nanosatellite: A tool for thermal barrier coating selection

LA Reyes, R Cabriales-Gómez, CE Chávez… - Applied Thermal …, 2020 - Elsevier
Abstract The effect of Thermal Barrier Coatings (TBC) and Orbital Elements (OE) and their
impact in the internal temperature of a CubeSAT type nanosatellite (named CIIIASat) were …

A dual-system cooperative co-evolutionary algorithm for satellite equipment layout optimization

FZ Cui, ZZ Xu, XK Wang, CQ Zhong… - Proceedings of the …, 2018 - journals.sagepub.com
This paper develops a new dual-system cooperative co-evolutionary algorithm for multi-
modules (or multi-bearing plate) satellite equipment layout optimization problem, based …

Analysis of the thermal design of a COTS-based modular battery system for satellites by thermal vacuum testing

M Eilenberger, H Gunasekar, D Gomez Toro… - CEAS Space …, 2024 - Springer
The qualification of components for satellite applications is a costly process due to the
extreme conditions that must be endured in space. Therefore, space market access of …

Design optimization of thermal paths in spacecraft systems

KD Stout - 2013 - dspace.mit.edu
This thesis introduces a thermal design approach to increase thermal control system
performance and decrease reliance on system resources, eg, mass. Thermal design …

Fuzzy-based analysis of thermal effects on component failure for LEO satellites

S Mengqi, Y Xinqing, L Guiming… - 2021 IEEE 2nd …, 2021 - ieeexplore.ieee.org
Thermal control is a key factor in protecting the low earth orbit satellites from the severe
space environment and thermal uncertainties throughout their lifetime. However, the exact …

Experimental evaluation of thermal simulation model for lunar exploration rover

T Oikawa, J Walker, K Yoshida - 2015 IEEE/SICE International …, 2015 - ieeexplore.ieee.org
In outer space, the environment is defined by complete vacuum and radiation in high energy
sources such as magnetic radiation, space particles, and cosmic rays. For these extreme …

Optimización del diseño para el control térmico pasivo de un nanosatélite mediante un algoritmo genético

ES Escobar Lavín - 2016 - repositorio.uchile.cl
El presente trabajo estudia el uso de algoritmos genéticos para automatizar el diseño del
sistema de control térmico pasivo de un nanosatélite tipo CubeSat de 3U en una …