Integral deployment Systems “KosmoLab” for light Launch Vehicles and interorbital small Upper-Stages are intended for placement and deployment of main Satellite as a Primary PayLoad. Also, the construction of Systems, consisted of integrated Deployers “KosmoLab”, provides placement and cluster deployment of CubeSats as a Secondary PayLoads.
Such integral construction of System provides sufficient rigidity and reduced mass characteristics compare to classical solutions.
Technical parameters of Deployment Systems “KosmoLab”:
| Mass of main Sattelite, kg | up to 300 |
| Mass of CubeSats, kg | up to 96 |
| Dimension-types of CubeSats | 1U – 16U |
| Mass of System (aluminum), kg Mass of System (composite), kg | not more than 60 not more than 40 |
Available modification of Systems according to your requirements specification and interface adjustment to desired launch vehicles.