Elastic Deployable Composite Tubular Roll-Out Boom

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX10CD62P
Agency Tracking Number: 095446
Amount: $99,843.00
Phase: Phase I
Program: SBIR
Awards Year: 2010
Solicitation Year: 2009
Solicitation Topic Code: S1.06
Solicitation Number: N/A
Small Business Information
955 Nysted Drive, Solvang, CA, 93463-2247
DUNS: 825308732
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Brian Spence
 Principal Investigator
 (805) 693-1319
 Brian.Spence@DeployableSpaceSystems.com
Business Contact
 Brian Spence
Title: Business Official
Phone: (805) 693-1319
Email: Brian.Spence@DeployableSpaceSystems.com
Research Institution
N/A
Abstract
DSS's innovative Elastic Deployable Composite Tubular Roll-Out Boom will provide revolutionary performance when compared to conventional state-of-the-art technologies, and will significantly enhance operations and capability for future NASA missions. The proposed Roll-Out Boom is strong, stiff, lightweight, thin, scalable, compactly-stowed, and fabricated from ultra-lightweight composite materials. The Roll-Out Boom can be used as a self-deploying antenna, electric field antenna, linear actuator, grapple arm, gravity gradient boom, camera support, inspection aid, or as an actuator/structure for deploying payloads, antennas, solar arrays, instrument benches, solar sails, and sunshades. The Roll-Out boom is a very simple concept that integrates an innovative deployment synchronization system to provide controlled, reliable and repeatable deployments, to produce deployments always in a predictable/known direction. The Roll-Out Boom provides exceptional structural performance in a small lightweight package, and is a direct replacement to current state-of-the-art systems. Boom sizes envisioned can be from 0.5-inch to 12-inches in diameter (or greater), with lengths from 1-m to 50-m long (or longer). The significance of the proposed technology and program will enable future NASA and non-NASA missions by providing a revolutionary and positive performance impact to the end-user, and allow for the rapid insertion of this mission-enabling technology for future applications.

* Information listed above is at the time of submission. *

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