« Back to Index SNIPE
- Spacecraft Name
- SNIPE
- COSPAR ID
- 2023-072
- Launch Date
- 2023-05-25
- Spacecraft Description
- N/A
Thermal Analysis
- Analysis Object
- System
- Analysis Description
- The SNIPE satellite thermal model was build with over 2100 nodes as GMM by using Thermal Desktop. The TMM values were correlated with the thermal balance test using the genetic-algorithm-based multi-objective optimization algorithm NSGA-II.
- Software Used
-
References
- Kim et al. (2023)
Kim, Ji-Seok and Lee, Seonho and Kim, Hui-Kyung and Kim, Hae-Dong, "Thermal Model Correlation of SNIPE Satellite Using Genetic-Algorithm-Based Multi-Objective Optimization Method", Journal of Spacecraft and Rockets, 2023 , DOI: 10.2514/1.A35517