| Name | SINOD-D |
|---|---|
| Type | CubeSat |
| Units or mass | 2U |
| Organisation | SRI International |
| Institution | Company |
| Entity | Commercial |
| Nation | US |
| Manufacturer | AIVT by Terran Orbital |
| Operator | Terran Orbital |
| Launch brokerer | Tyvak, ? |
| Partners | Tyvak |
| Oneliner |
High-speed data downlink for via software defined radio. |
| Description |
High-speed data downlink for wide-bandwidth CubeSat payloads via software defined radio communications. |
| Sources | [1] [2] |
| COTS subsystems |
|
Related Spacecraft
| Name | Status | Launch | Orbit |
|---|---|---|---|
| SINOD-D 1 (SRI International NanoSat Orbital Demonstration) | Operational? (Lack of recent reports, but likely was operational and may still be as of 2023-06-09) | 2015-10-08 | 500 x 800 km, 64.8 deg |
| SINOD-D 3 (SRI International NanoSat Orbital Demonstration) | Operational? (Lack of recent reports, but likely was operational and may still be as of 2023-06-09) | 2015-10-08 | 500 x 800 km, 64.8 deg |
| SINOD-D 2 | cancelled | x_cancelled | cancelled |
Last modified: 2023-06-09
Detailed SINOD-D entry in the Database
Full Nanosats Database (much more data)
