| Spacecraft | CEPHEUS |
|---|---|
| Type | CubeSat |
| Units or mass | 3U |
| Status | cancelled |
| Organization | Solar MEMS (Test In Space) |
| Institution | Company |
| Entity type | Commercial |
| Headquarters | Spain |
| Partners | SolarMEMS, Inabensa, Idener, Alter Technology and Mesurex, Abengoa Hidrógeno |
| Oneliner |
Educational and research project with multiple payloads including fuel cell system. |
| Description |
Research project aimed to the development, construction and validation of a pico-satellite based on CubeSat standard from design phase to Flight Model (FM) phase. “Cepheus” pico-satellite embeds various experimental payloads, namely: fuel cell system, star tracker with MEMS (MicroElectroMecanical System) technology and secondary communications link. This way, the project faces some of the main challenges of current micro space vehicles: energy storage, navigation sensor cost, and communication link energy consumption. |
| Notes | |
| Sources | [1] |
| Photo sources | [1] |
Last modified: 2024-05-28
