SBIR/STTR Research Award

Advanced Solar Array for Dual Launch GPS

Award identifier bc9f6a047185cb0c8ebb46016960b32ecd81fa52ad97d557142b27240d665190Awarding agency Department of Defense · Air Force

Award amount

$720,961

Program and phase

SBIR · Phase II

Award year

2017

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
ANGSTROM DESIGNS INC
Proposal award date
2016-11-22
Contract end date
2019-01-14
UEI
PFJ8LV1Q7SF8
Solicitation number
15.1
Topic code
AF151-076

Research abstract

ABSTRACT: Solar arrays power the vast majority of space missions and solar arrays with higher power, better mass efficiency and improved packaging are critical, especially given recent interest in dual launching of GPS satellites. The Compact Telescoping Array (CTA) architecture is a very promising new technology. The backbone of the CTA wing is an extremely mass-efficient lattice truss telescoping boom where the photovoltaics are supported on flexible blankets that are Z-folded when stowed for volumetric efficiency. Compared to existing technology, construction is low cost due in part to the boom segments being composed of relatively inexpensive graphite-epoxy pultrusions. Phase I results show CTA to consistently deliver outstanding performance metrics over a broad range of power. CTA wings are lightweight, compact, and reliable and offer considerable cost savings. Phase II work is planned to include the design, analysis and construction of a mechanically functional CTA wing and vertically oriented offloading equipment. This prototype wing will be representative of a 10 kW two-wing system and will be capable of demonstrating all three phases of deployment. The wing will undergo various functional and environmental tests with the end goal of increasing the TRL of CTA to 5 or 6.; BENEFIT: With a successful completion of Phase II work, Angstrom Designs expects CTA to be in a position to compete favorably with existing solar array technologies. CTA could find application in both commercial and military sectors. With versions in the 1 to 5 kW range delivering great performance, CTA would be well-suited for the Air Force’s initiative of disaggregation. On the commercial side, two suppliers of commercial satellites, Orbital ATK and Boeing, are currently seeking to replace rigid panel technology with flexible blanket systems in their near term high power programs. Angstrom Designs believes that the CTA will be a top contender in this sector. Following Phase II work, we expect applications should be in the form of purchase contracts with our subcontractor and commercialization partner, Orbital ATK Goleta.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

18 SBIR/STTR records share this UEI (2012–2025). Reported award amounts total $8,258,744. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense

Agency intelligence

Department of Defense

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