SBIR/STTR Research Award

High Planer and Through-Thickness Conductivity Enhancement for Lightweight Isothermal Composite Satellite Panels

Award identifier 59c6af7a8fbe7e0f840b3ca7490711c7a1a4b0bb29382725e65e4d113a71f9d2Awarding agency Department of Defense · Air Force

Award amount

$100,000

Program and phase

SBIR · Phase I

Award year

2009

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
KaZaK Composites Incorporated
Proposal award date
2009-03-17
Contract end date
2010-03-17
UEI
NE6AZWKUS6Z7
Solicitation number
2008.3
Topic code
AF083-217

Research abstract

KaZaK Composites, supported by a diverse team of in-house and subcontractor experts in materials, processing, thermal design and satellite structures, will develop and demonstrate a cost-effective, lightweight isothermal satellite panel that integrates a range of interrelated technologies to ensure a uniform temperature field both across and through the thickness of satellite bus structure. The proposed solution involves creation of an advanced 3D fabric with highly conductive pitch-based carbon fibers. 3D fabric will provide Z-direction continuity via mini thermal paths created by through-thickness fibers. Inter-panel connections will be reduced by folding one continuous sheet of fabric to form the main satellite bus. Thermal contact resistance of the smaller number of remaining inter-panel connections will be minimized using advanced fillers and fastening techniques. All surfaces will be polished and coated to expose fibers on panel faces and edges.  In Phase I, KaZaK will focus on analytical design of flat plate thermal panels, prototype fabrication and thermal testing. Data will demonstrate thermal performance of both panels and inter-panel connections. Results will provide the Air Force with sufficient confidence in the concept to move forward into Phase II, where full scale demonstration using our proposal partners spacecraft bus structure will occur. BENEFIT: A novel design and manufacturing process for creation of isothermal satellite panels will enhance the ability of future high performance systems to access technology that provides high thermal conductivity in all directions, including in-plane, through-thickness and across inter-panel joints. KaZaKs solution could be employed by commercial satellite makers such as MicroSAT Systems, who has expressed direct interest in and support of KaZaKs solution. Larger spacecraft and aircraft manufacturers such as Lockheed Martin, Raytheon, Northrop Grumman, and Boeing, as well as the computer/electronic chip packaging industry, could exploit the lightweight, high thermal conductivity and good structural properties of KaZaKs proposed solution in a variety of applications where these features are important. Possible alternative applications include circuit boards, heat spreaders, heating and cooling systems, and missile bodies.

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

156 SBIR/STTR records share this UEI (1995–2011). Reported award amounts total $40,421,900. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Transportation, National Science Foundation

Agency intelligence

Department of Defense

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