Topic
Computational verification of satellite structural design feasibility under launch environment conditions.
Random Vibration Profile
1 minute for each axis
Orbit Definition
- Eccentricity : 0.007217
- Semi-major axis : 7028.1km (Altitude 500~600km)
- Inclination : 1.71 rad (98 deg, TBD)
- Longitude of the ascending node : 2.88 rad (LTAN 11h-TBC)
- Argument of periapsis : 3.40 rad
- Mean anomaly : 0 rad
S/C Attitudes Relevant to Thermal Analysis
- Orientation type : Spin aligned
- Aligned vector : X axis
- Constrained vector : Toward Nadir
- Angular velocity : 0.035 rad/s
FEA Results
- Quasi-static load analysis
- Natural vibration analysis
- Random vibration analysis
- On-orbit thermal analysis
Funding
Korea Test Laboratory (KTL)