Roccor, LLC

Composite Technology Development, Inc.

Mark S Lake

William H Francis

Dana Turse

Robert Taylor

Gregg E Freebury

Neal J Beidleman

Michael Hulse

Philip N Keller

Thomas J Rose

Bruce L Davis

Steven Isaacs

Will Francis

Rory Barrett

Greg Shoukas

Philip Keller

Kellie A Craven

Mario Saldana

William Brad Hensley

Kaushik Mallick

Naseem A Munshi

John Cronin

Diego Arias

Kevin Cox

Mark Warner

Systems, devices, and methods for precision boom deployment are provided in accordance with various embodiments. The tools and techniques provided may have space and/or terrestrial applications. Some embodiments include a boom deployment system that may include a furlable boom. Some embodiments include: boom reinforcement devices, end fitting devices, contoured support devices, edge support devices, spiral harness devices, latch devices, combined boom spool and tension drive devices, and/or rotary encoder devices. Some embodiments may utilize a composite slit-tube boom. Some embodiments utilize a furlable boom that may be fabricated with curvature along its length.

Precision deployment devices, systems, and methods

Passively deployable thermal management devices, systems, and methods are provided in accordance with various embodiments. For example, some embodiments include a passively deployable radiator device that may include: one or more thermally conductive layers; and/or one or more strain energy components configured to deploy passively the one or more thermally conductive layers. The one or more thermally conductive layers may include one or more carbon layers. The one or more carbon layers may include at least one or more graphite layers or one or more graphene layers. At least the one or more graphite layers or the one or more graphene layers include at least one or more pyrolytic graphite sheets or one or more pyrolytic graphene sheets.

Passively deployable thermal management devices, systems, and methods

An extendible membrane system may include: an extendible central column; one or more membranes; and/or one or more foldable membrane supports configured to support the one or more membranes. Each of the one or more foldable membrane supports may be configured to extend from the extendible central column. In some embodiments, one or more of the one or more foldable membrane supports includes two or more segments that may be configured to couple with each other. A method of deploying one or more membranes may include unfolding one or more foldable membrane supports from a folded configuration to a linear configuration. An extendible membrane device may include one or more membranes and one or more foldable membrane supports configured to support the one or more membranes.

Extendible membrane systems, devices, and methods for space applications

Devices, systems, and methods for flexible, deployable structures with optical fiber are provided in accordance with various embodiments. For example, some embodiments include a system that may include a flexible, deployable structure and one or more optical fibers coupled with the flexible, deployable structure. In some embodiments, one or more conditions of the one or more optical fibers coupled with a flexible, deployable structure may be determined. One or more conditions of the flexible, deployable structure may be determined utilizing the determined one or more conditions of the one or more optical fibers coupled with the flexible, deployable structure. The one or more conditions of the one or more optical fibers may be correlated to the one or more conditions of the flexible, deployable structure.

Devices, systems, and methods for flexible, deployable structure with optical fiber

Methods, systems, and device for two-phase thermal management are provided in accordance with various embodiments. For example, some embodiments include a two-phase thermal management device that may include: a liquid chamber; one or more inlets configured to deliver a liquid to the liquid chamber; an evaporator chamber; a capillary layer positioned within the evaporator chamber and configured to spread the liquid from the liquid chamber; a liquid manifold configured to deliver the liquid from the liquid chamber to at least the capillary layer or the evaporator chamber; and/or one or more outlets configured to remove at least a vapor or a portion of the liquid from the evaporator chamber. Some embodiments that may include a two-phase thermal management device coupled with at least: a heat exchanger, a pump, a heat recuperator, a pre-heater, and/or a variable volume reservoir. Some embodiments include a two-phase thermal management method.

Two-phase thermal management devices, systems, and methods

A linerless tank structure has a body that defines an enclosed interior volume. The body has a cylindrical section having an axis of symmetry and a dome section coupled with the cylindrical section. The construction of the pressure vessel includes multiple fiber plies. At least one of the fiber plies is a helical ply having fibers traversing the dome helically about the axis of symmetry. At least a second of the fiber plies is a braided or woven ply.

Damage and leakage barrier in all-composite pressure vessels and storage tanks

A deployable structure is disclosed. The deployable structure may include one or more slit-tube longerons; and one or more flat sheets coupled with the one or more slit-tube longerons. The one or more slit-tube longerons and the one or more flat sheets may be stowed by rolling the one or more slit-tube longerons and the one or more flat sheets together into a roll. In one embodiment, at least a portion of the one or more slit-tube longerons may be exposed when stowed. In another embodiment, the one or more slit-tube longerons may be manufactured from a shape memory material. These slit-tube longerons unroll into to a straight configuration when exposed to heat.

Large-scale deployable solar array

Growing community of inventors

Erie, CO, United States of America

Mark S Lake