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
Systems can be modified according to requirements specification (Acceleration parameters, Mass of Primary PayLoad, second Deployers’ level, etc.) for particular Launch Vehicle.