| Satellite | AMDROHPSat (AMDROPHSat, Additively Manufactured Deployable Radiator with Oscillating Heat Pipes) |
|---|---|
| Form factor | CubeSat |
| Units or mass | 3U |
| Status | not launched, expected in 2026 |
| Launcher | Falcon 9, (Cygnus), (NG-25) |
| Organisation | California Polytechnic State University (Cal Poly) |
| Institution | University |
| Entity | Academic / Education |
| Nation | US |
| Operator | In-house? |
| Oneliner |
Demonstrate the use of a new generation of deployable radiators. |
| Description |
Additively Manufactured Deployable Radiator with Oscillating Heat Pipes (AMDROHPSat) primary aim is to demonstrate the use of a new generation of deployable radiators in low-Earth orbit (LEO). The demonstration of this technology will enable small satellite mission with greater thermal constraints to operate in LEO and beyond. |
| Notes | |
| Sources | [1] [2] [3] |
| Photo sources | [1] |
Last modified: 2026-08-01
