« Back to Index Hodoyoshi 1
- Spacecraft Name
- Hodoyoshi 1
- COSPAR ID
- 2014-070B
- Launch Date
- 2014-11-06
- Spacecraft Description
- Hodoyoshi-1 is a micro stellite that is about 60 cm cube and 60kg.
Thermal Analysis
- Analysis Object
- System
- Analysis Description
- The external surface of the satellite is Alodine 1000. The satellite internal structures are black anodized. Between the external structure and internal structure, thermal isolators (glass epoxy) are inserted, so that the internal instruments are not directly influenced by the external structure's temperature variations.
Regrading the thermal anlysis, one-node and two-node analysis were performed with Fortran, and multi-node thermal analysis was performed with Thermal Desktop.
- Software Used
-
- Fortran
- Thermal Desktop Version 4.8
References
- Ogawa et al. (2012)
Hiroto Ogawa and Ryota Inoue and Tsuyoshi Totani and Masashi Wakita and Harunori Nagata, "Thermal design of the micro-satellite"HODOYOSHI-1" (in Japanese)", 2012, 2012 , DOI: 10.1299/jsmemecj.2012._S192013-1