Research Article
Design and Implementation of 3U CubeSat Platform Architecture
Table 4
KAUSAT-5 system specification.
| Item | Description |
| Mission orbit | Sun synchronous elliptical orbit: 450 km × 720 km Inclination: 98° | Mission lifetime | >1 year | CubeSat dimension | 100 × 100 × 340 mm3 | Payload | IR camera, GMRM, VSCMG, FLCMPPT | Payload mass | IRC mass: 580 g GMRM mass: 47 g | IR camera | Resolution: 320 × 240 (m)FOV: 13.5 deg. | GMRM | Resolution: >18 CPS/mR/h Accuracy: <3 mR/h | Spacecraft mass | <4 kg | Satellite power | <6.4 W @ EOL (nadir) <13 W @ EOL (sun pointing) | ADCS | 3-axis stabilization Accuracy: <0.88 deg. Knowledge: <0.87 deg. Stability: <0.42 deg/s | Link margin | >3 dB @ 10 deg. elevation angle | Data rate | UHF downlink: 9600 bps VHF uplink: 1200 bps S-band downlink: 115,200 bps |
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