thermal orbital heating rates lapan-tubsat analysis using software thermal desktop 5.0 and sinda/fluint 5.0
- Paper number
IAC-08.C2.7.6
- Author
Mr. Ahmad Fauzi, National Institute of Aeronautics and Space (LAPAN), Indonesia
- Year
2008
- Abstract
LAPAN-TUBSAT is the first microsatellite owner by LAPAN {Indonesian National Institute of Aeronautics and Space}. LAPAN-TUBSAT satellite has experienced in test fly by carrying the surveillance mission or perception from air. This satellite at the same time is mean to study the bus system a microsatellite. In this paper, will be presented about concerning thermal satellite condition of LAPAN-TUBSAT in orbit, the solution are consists of the simulation orbit and the thermal orbital heating rates LAPAN-TUBSAT microsatellite temperature. The result from graphic that known the distribution temperature of body mounted satellite which hot case need next control.
- Abstract document
- Manuscript document
(absent)