M.m.a. Design, LLC

Timothy John Ring

Thomas Jeffrey Harvey

Colleen Roseanna Harvey

Susan Christine Tower

An antenna system for space applications provides a membrane antenna with one or more flexible membranes. An antenna enclosure stores the membrane antenna during stowage. One or more first deployable support structures extend along a first axis from the antenna enclosure during deployment, at least a first point of the membrane antenna being operably anchored to a point on the first deployable support structures. Deployment mechanisms are operably anchored at a junction with the first deployable support structures. The deployment mechanisms extend one or more second deployable support structures along a second axis from the first deployable support structures during deployment. At least a second point of the membrane antenna is operably anchored to a point on the second deployable support structures. Extension of the first deployable support structures and second deployable support structures unfurls the membrane antenna along both axes to overlap the junction.

Multi-direction deployable antenna

A deployable boom structure is provided that, in one embodiment, includes one or more perforated tapes, a drive mechanism with a sprocket mechanism for engaging each of the perforated tapes to transition the tapes between an undeployed state and a deployed state, and three battens that each extend between the tapes. At least one of the battens is a sliding batten, i.e., a batten that engages each of the tapes but through which each of the tapes can slide. Lanyards and detents cooperate to fix the location of a sliding batten relative to the tapes after a predetermined length of each of the tapes has slid through the batten. In a particular embodiment, the deployable boom structure is coupled with a solar blanket that can be Z-folded.

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Louisville, CO, United States of America

Timothy John Ring