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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