Responsive Secondary Payload Launch

This effort will develop the power, communication and launch vehicle (LV) interface systems of a parasitic "drone" satellite to be used in close proximity with a host satellite. The power system will harvest energy from the side lobes of the host satellite's microwave transmissions. The communication system will transfer data with the host through that same microwave frequency, negating the need for a second communication system on the host spacecraft. The launch vehicle interface will be a responsive and non-intrusive separation system that requires no electrical connections with the LV and bonds on to the structure late in the integration cycle. The interface accommodates both controlled separation as well as redocking maneuvers; it also has the capability to transfer power to the drone if the choice is made to run power lines to it. The interface can bonded to either the LV or the host spacecraft as the individual mission requires.