| Spacecraft |
HYVRID |
| Spacecraft type |
CubeSat |
| Units or mass |
3U |
| Status |
Operational? (No information found and SatNOGS is inconclusive, last checked 2025-04-20) |
| Launched |
2025-03-15 |
| NORAD ID |
? |
| Deployer |
EXOpod Nova 12U/16U [Exolaunch] |
| Launcher |
Falcon 9 (Transporter-13) |
| Entity name |
Yonsei University |
| Institution |
University |
| Entity type |
Academic / Education |
| Headquarters |
South Korea |
| Oneliner |
Equipped with a thin film deployment device.
|
| Description |
- CubeSat recognizes lasers fired from the ground through a laser recognition module and transmits the results to the ground through a communication module.
- To this end, the sensor of the laser recognition module was developed to reliably recognize the wavelength of the SLR laser and the orbital reception output.
- CubeSat is equipped with a thin film deployment device to simulate the shape that can be tracked by the optoelectronic system for precise tracking of space objects.
- To operate the laser recognition module and thin film deployment device as payloads, a cube satellite bus system of at least 3U size is configured.
- The CubeSat bus system includes a camera and an attitude control module for Earth orientation.
- Because the image information is large in size, it is transmitted to the ground using S-band communications.
- Precise orbit determination is performed through ground postprocessing based on GPS L1 and L2 information.
|
| Sources |
[1] |
| Photo sources |
[1] |
| On the same launch |
|
Last modified: 2025-04-26
