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![슬라이드1.PNG](https://static.wixstatic.com/media/ff64c5_0438ae1a701644379c7608f70141f99a~mv2.png/v1/fill/w_960,h_719,al_c,q_90,enc_avif,quality_auto/%EC%8A%AC%EB%9D%BC%EC%9D%B4%EB%93%9C1_PNG.png)
SNUGLITE-III Project
The 3rd CubeSat
![concept.jpg](https://static.wixstatic.com/media/ff64c5_a6089499f9424650b3ea5ca20df058b3~mv2.jpg/v1/fill/w_940,h_299,al_c,lg_1,q_80,enc_avif,quality_auto/concept.jpg)
SNUGLITE-II Project
Launch: 21st June 2022 (Nuri, KSLV-II, Korea)
The 2nd CubeSat
Main: 환영
![intro_SNUGLITE.png](https://static.wixstatic.com/media/ff64c5_9fbedba6951645ab98dab8fd4802bb4c~mv2.png/v1/fill/w_940,h_529,al_c,q_90,usm_0.66_1.00_0.01,enc_avif,quality_auto/intro_SNUGLITE.png)
Main: Welcome
SNUGLITE-I CubeSat
- Platform: 2U CubeSat
- Main payloads: L1/L2C GPS receiver x2
- Sub payloads:
3-axis fluxgate magnetometer w/ deployable boom
- Mass: 1.9 kg
- Orbit: SSO 575km (LTDN 10h30m)
- Frequency:
> UHF (437.275MHz)
* downlink : beacon, command-return
* uplink : tele-command
> S-band (2405MHz)
* downlink : housekeeping data, mission data
![DSC05981.JPG](https://static.wixstatic.com/media/ff64c5_17759bd0bb0d44c298e93090d35f9af9~mv2_d_6000_4000_s_4_2.jpg/v1/crop/x_2623,y_222,w_2555,h_3777/fill/w_460,h_680,al_c,q_80,usm_0.66_1.00_0.01,enc_avif,quality_auto/DSC05981_JPG.jpg)
The 1st CubeSat
Main: 헤드라인
Recent Posts
Main: 블로그 피드
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