| Name | NanoACE |
|---|---|
| Type | CubeSat |
| Units or mass | 3U |
| Status | Operational? (Tyvak paper in CubeSat Developers Workshop 2018 but no news since then for the past 5 years, could be retired) |
| Launched | 2017-07-14 |
| NORAD ID | 42844 |
| Deployer | EXOpod 12U/16U [Exolaunch] |
| Launcher | Sojuz-2-1a |
| Organisation | Tyvak |
| Institution | Company |
| Entity | Commercial |
| Nation | US |
| Manufacturer | AIVT by Terran Orbital |
| Launch brokerer | Exolaunch |
| Oneliner |
Validate CubeSat platform technologies and test propulsion module plus cameras. |
| Description |
Validate the Endeavor suite technologies that will be used for future missions and is solely for the purpose of internal Tyvak development as an attitude control experiment. Includes VACCO propulsion module. Validate the Command and Data Handling (CDH) system, Guidance Navigation and Control (GNC) software and actuators, as well as test visible & IR cameras. |
| Sources | [1] [2] |
| Photo sources | [1] |
| COTS subsystems |
|
| Keywords | Propulsion |
Last modified: 2023-06-09
Detailed NanoACE entry in the Database
Full Nanosats Database (much more data)
