| Name | TechEdSat-3p |
|---|---|
| Type | CubeSat |
| Units or mass | 3U |
| Status | Reentry 2014-01-16. Was operational (Successfully performed the first passive Exo-Brake test. DK3WN wrote as it was never heard from). |
| Launched | 2013-08-03 |
| NORAD ID | 39415 |
| Deployer | J-SSOD (JEM Small Satellite Orbital Deployer) |
| Launcher | H-IIB (H2B) |
| Organisation | Space agency |
| Organisation | NASA Ames Research Center |
| Nation | US |
| Oneliner | Demonstrate drag device deorbiting system and Iridium modem. |
| Keywords | Globalstar or Iridium or Inmarsat, De-orbit device |
Last modified: 2019-07-13
Detailed TechEdSat-3p entry in the Database
Full Nanosats Database (much more data)
