A satellite apparatus is disclosed, including a housing having first and second opposing walls, and a support structure inside the housing spanning the first and second walls. The support structure is structurally connected to the housing only at the first and second walls, and an end portion of the support structure is configured for connection to a launch vehicle by a separation system.
Stacked satellite assemblies and related methods
2025-06-03
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |