Affordable Practical High-Efficiency Photovoltaic Concentrator Blanket Assembly for Ultra-Lightweight Solar Arrays

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX12CA22C
Agency Tracking Number: 105538
Amount: $749,681.00
Phase: Phase II
Program: SBIR
Awards Year: 2012
Solicitation Year: 2010
Solicitation Topic Code: S3.03
Solicitation Number: N/A
Small Business Information
Deployable Space Systems, Inc.
CA, Goleta, CA, 93117-3108
DUNS: 825308732
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Brian Spence
 Principal Investigator
 (805) 693-1313
 Brian.Spence@DeployableSpaceSystems.com
Business Contact
 Brian Spence
Title: Business Official
Phone: (805) 693-1313
Email: Brian.Spence@DeployableSpaceSystems.com
Research Institution
 Stub
Abstract
Deployable Space Systems, Inc. (DSS) will focus the proposed NASA Phase 2 effort on the development and TRL 5/6 maturation of our innovative Functional Advanced Concentrator Technology (FACT) for standard multi-junction and advanced IMM photovoltaics. FACT is a highly-affordable, practical, high-efficiency, ultra-lightweight photovoltaic concentrator blanket assembly that can be rolled or z-folded in a stowed configuration. FACT coupled to an ultra-lightweight solar array structural platform will provide game-changing performance metrics and unparalleled affordability. FACT will enable emerging SEP Space Science and Exploration missions through its ultra-affordability, ultra-lightweight, ultra-compact stowage volume, and practical/user-friendly off-pointing versus power characteristics. The FACT technology promises to provide NASA/industry a near-term and low-risk flexible blanket technology for advanced solar array systems. The FACT technology provides revolutionary performance in terms of: High specific power (>260W/kg BOL with ZTJ/XTJ and ~400W/kg BOL with IMM PV when coupled to ROSA-array); Affordability (>40% cost savings when coupled to ROSA-array); Flexible blanket compatibility / architecture flexibility (accommodates rolled or z-folded blankets); User-friendly off-pointing versus power characteristics; Compact stowage volume (>50kW/m3); High deployment reliability; High radiation tolerance and high voltage operation capability; Applicability/scalability to many missions (500W-1MW+ sizes); LILT/HIHT operation capability; and Adaptable to standard rigid honeycomb panel arrays.

* information listed above is at the time of submission.

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