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A Multifunctional Hypersonic Leading Edge with Integrated Thermal Management

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: 80NSSC19C0425
Agency Tracking Number: 193896
Amount: $124,998.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: A1
Solicitation Number: SBIR_19_P1
Timeline
Solicitation Year: 2019
Award Year: 2019
Award Start Date (Proposal Award Date): 2019-08-19
Award End Date (Contract End Date): 2020-02-18
Small Business Information
2508 Paris Road, Columbia, MO, 65202-2514
DUNS: 808369792
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Daniel Pounds
 (573) 397-6912
 daniel.pounds@thermavant.com
Business Contact
 Alex Miller
Phone: (573) 321-4554
Email: alex.miller@thermavant.com
Research Institution
N/A
Abstract
In response to NASA SBIR FY 2018 topic A1.10, Hypersonic Technology, ThermAvant Technologies, LLC (ThermAvant) proposes to develop a high temperature, conformal thermal-mechanical leading edge skin for hypersonic aircraft. The proposed structure will provide high temperature, high heat flux acquisition and dissipation, as well as providing the structural integrity required to meet mission objectives. ThermAvant#39;s research team will demonstrate the proposed concepts and innovations through design, manufacturing and laboratory testing.In response to NASA SBIR FY 2018 topic A1.10, Hypersonic Technology, ThermAvant Technologies, LLC (ThermAvant) proposes to develop a high temperature, conformal thermal-mechanical leading edge skin for hypersonic aircraft. Specifically, the proposed structure will provide high temperature, high heat flux acquisition and dissipation, as well as providing the structural integrity required to meet stringent mission objectives. ThermAvant#39;s research team will demonstrate the proposed concepts and innovations through design, manufacturing and laboratory testing.

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

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