TechEdSat 9 (Technical and Educational Satellite 9) is a 3U CubeSat. It was built as a conjoined project between San Jose State University (SJSU) and the University of Idaho as a collaborative engineering project, with oversight from the NASA Ames Research Center.
The TechEdSAT-9 will test automatic deorbiting using the Exo-Brake system.
A launch opportunity has not yet been announced, although a launch on the maiden flight of Virgin Orbit's LauncherOne was considered.
| Nation: | USA |
|---|---|
| Type / Application: | Technology, education |
| Operator: | SJSU, University of Idaho, NASA Ames Research Center |
| Contractors: | SJSU, University of Idaho, NASA Ames Research Center |
| Equipment: | Exo-Brake |
| Configuration: | CubeSat (3U) |
| Propulsion: | None |
| Power: | Solar cells, batteries |
| Lifetime: | |
| Mass: | |
| Orbit: |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| TechEdSat 9 (TES 9) | - | 202x | with ? |
