SBIR/STTR Research Award

Nano Enhanced 4000 °F CMC for Multiple Use Applications

Award identifier 196a3896c69202277631640a5d0e4de9797e6a4cee24f69853e757a4035c981dAwarding agency National Aeronautics and Space Administration

Award amount

$749,295

Program and phase

SBIR · Phase II

Award year

2019

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Allcomp Inc.
Proposal award date
2019-08-14
Contract end date
2021-08-13
UEI
D55JVDSPY5K5
Solicitation number
SBIR_18_P2
Topic code
H5

Research abstract

NASA future applications require non- incremental advances in high temperature materials.nbsp; Specifically, advanced future propulsion systems require significant improvement in the upper temperature operating limit of composite materials.nbsp;Carbon-carbon (C-C) composites exhibit unique properties on increasing strength with temperature but suffer from oxidation at temperatures above 550 C.nbsp; Over the years significant efforts in the oxidation protection ofnbsp;C-C compositesnbsp; included internal inhibition, external coatings and sealants.nbsp;The reliability of such oxidation protection system is greatly limited by the intrinsic risk of coating spallation.nbsp; On the other hand the internal inhibition by itself is incapable of providing sufficient substrate protection at high temperatures without the external coatings.nbsp;Phase I results provided initial paradigm shift into the feasibility of internal oxidation protection system for 3500 F to 4200 F applications.This Phase II builds on very encouraging and insightful Phase I results and provides for a comprehensive, unique molecular level inhibition of the fiber, intrabundle matrix and interbundle matrix.nbsp; System chemistry will be optimized to offer NASA a plethora of opportunities in such demanding applications as extension nozzles and combustors offering max temp operation up to 4,200 F with the material system chemistry and molecular inhibition design enabling the composite based parts to experience very large temperature gradients and providing effective oxidation protection of the substrate.nbsp;nbsp;In short, the uniqueness of this molecular inhibition system, based on Allcomprsquo;s provisional patent, eliminates the need for external coatings and sealants. By the elimination of the external coatings the huge coating spallation reliability problem will be solved offering a paradigm shift applicable not only to NASA propulsion applications but the plethora of other NASA applications, military, and commercial applications.

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.

Research funding history

62 SBIR/STTR records share this UEI (1999–2020). Reported award amounts total $22,355,305. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy

Agency intelligence

National Aeronautics and Space Administration

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