| Name | TechEdSat-10 (TES-10) |
|---|---|
| Type | CubeSat |
| Units or mass | 3U |
| Status | Reentry 2021-03-15. Was operational? (No public sources found directly stating it is operational as of 2020-12-15, but exo-brake was deployed right after launch as seen from photos) |
| Launched | 2020-02-14 |
| NORAD ID | 45917 |
| Deployer | NRCSD-E (External NanoRacks CubeSat Deployer) |
| Launcher | Antares (ELaNa 30) |
| Deployment | Deployed from ISS on 2020-07-13 |
| Organisation | NASA Ames Research Center |
| Institution | Space agency |
| Entity | Government (Civil / Military) |
| Nation | US |
| Launch brokerer | NASA CSLI / ELaNa |
| Oneliner |
High temperature, accurate deorbit reentry nanosatellite. |
| Results |
Successfully demonstrated Exo Brake modulation effect on drag, along with all payloads and avionics. |
| Sources | [1] [2] [3] |
| Photo sources | [1] [2] [3] |
| Keywords | Globalstar or Iridium or Inmarsat, De-orbit device |
| Space photos | 
|
Last modified: 2023-06-03
Detailed TechEdSat-10 entry in the Database
Full Nanosats Database (much more data)
