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Flexible TPS

Award Information
Agency: Department of Defense
Branch: Missile Defense Agency
Contract: HQ0860-21-C-7030
Agency Tracking Number: B202-007-0142
Amount: $149,998.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: MDA20-007
Solicitation Number: 20.2
Timeline
Solicitation Year: 2020
Award Year: 2021
Award Start Date (Proposal Award Date): 2020-12-28
Award End Date (Contract End Date): 2021-06-30
Small Business Information
20 New England Business Center
Andover, MA 01810-1111
United States
DUNS: 073800062
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 John Steinbeck
 (978) 738-8148
 jws@psicorp.com
Business Contact
 B. David Green
Phone: (978) 689-0003
Email: green@psicorp.com
Research Institution
N/A
Abstract

The Physical Sciences Inc. (PSI) Team will develop ultrathin (0.015”) carbon fiber reinforced, silicon carbide matrix (C/SiC) materials to construct flexible thermal protection system (TPS) structures. The natural oxidation resistance of C/SiC makes these flexible structures suitable for use as control surfaces or morphing ducts for hypersonic vehicles. The key innovation developed by PSI to make repeatable thin C/SiC structures possible is a shape stable matrix. The thin C/SiC sheets are reinforced by unidirectional tapes in a simple 0-90 scheme. During the Phase I program we will fabricate thin C/SiC sheets and demonstrate their ability to bend about a 12” radius of curvature. We will assemble a set of eight thin sheets and show that the stack can be actuated about a 12” radius of curvature and that the thermal performance of the assembly is within 25% of a monolithic C/SiC structure. Our Team will work with the government and vehicle integrators to identify an application for the flexible structures for prototype development during Phase II. The Physical Sciences Inc. (PSI) Team will develop ultrathin (0.015”) carbon fiber reinforced, silicon carbide matrix (C/SiC) materials to construct flexible thermal protection system (TPS) structures. The natural oxidation resistance of C/SiC makes these flexible structures suitable for use as control surfaces or morphing ducts for hypersonic vehicles. The key innovation developed by PSI to make repeatable thin C/SiC structures possible is a shape stable matrix. The thin C/SiC sheets are reinforced by unidirectional tapes in a simple 0-90 scheme. During the Phase I program we will fabricate thin C/SiC sheets and demonstrate their ability to bend about a 12” radius of curvature. We will assemble a set of eight thin sheets and show that the stack can be actuated about a 12” radius of curvature and that the thermal performance of the assembly is within 25% of a monolithic C/SiC structure. Our Team will work with the government and vehicle integrators to identify an application for the flexible structures for prototype development during Phase II. Approved for Public Release | 20-MDA-10643 (3 Dec 20)

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

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