« Back to Index AlAinSat-1
- Spacecraft Name
- AlAinSat-1
- COSPAR ID
- N/A
- Launch Date
- 2025-01-14
- Spacecraft Description
- N/A
Thermal Analysis
- Analysis Object
- System
- Analysis Description
- The meshed thermal model of AlainSat-1 consists of 20816 elements. Using a workstation Windows 10 Enterprize woth 3.10 GHz Intel Core i9-9900 and 8 GB RAM, a steady state thermal analysis takes 3–5 min, and a transient thermal analysis takes 1–2 hours to reach convergence.
- Software Used
-
References
- Seyedzadeh et al. (2025)
Ameereh Seyedzadeh and Mohamed Okasha and Alia Alblooshi and Wan Faris Aizat and Abdul Halim Jallad and Erwin Sulaeman, "Thermal analysis and experimental validation of the thermal subsystem of AlAinSat-1", The Egyptian Journal of Remote Sensing and Space Sciences, 2025 , DOI: https://doi.org/10.1016/j.ejrs.2025.03.002