Systems for Separating Small, Medium, Heavy Spacecraft

The ‘Systems for Separating Small, Medium, Heavy Spacecraft’ are engineered for the design, manufacture, and testing of spacecraft separation mechanisms. These systems facilitate the release of spacecraft from their launch vehicle mounts, which typically involve quick-disconnect devices such as locks and pyro-bolts. To prevent the spacecraft from colliding with the detached part of the launch vehicle, the separation system incorporates exciters (e.g., pushers, nozzles, engines). These exciters ensure the spacecraft’s departure from the launch vehicle without damage and with minimal disturbances. Such disturbances can arise from the attachment points, as locks, power activators, and communication connectors not only provide separation but also generate impulses of force and moment acting on the spacecraft. The product is flight-qualified and can be adapted to meet specific customer requirements, leveraging extensive work experience in this field.