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S. D. MILLER AND ASSOCIATES P.L.L.C. SBIR Phase I Award, August 2020

A SBIR Phase I contract was awarded to S. D. MILLER AND ASSOCIATES P.L.L.C. in August, 2020 for $124,998.0 USD from the NASA.

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sbir.gov/node/1882317
Is a
SBIR/STTR Awards
SBIR/STTR Awards

SBIR/STTR Award attributes

SBIR/STTR Award Recipient
‌
S. D. MILLER AND ASSOCIATES P.L.L.C.
0
Government Agency
NASA
NASA
0
Award Type
SBIR0
Contract Number (US Government)
80NSSC20C06670
Award Phase
Phase I0
Award Amount (USD)
124,9980
Date Awarded
August 20, 2020
0
End Date
March 1, 2021
0
Abstract

While working on NASArsquo;s Convective Heating Improvement for Emergency Fire Shelters (CHIEFS) effort, S. D. Miller amp;nbsp;Associates (SDMA) developed methods of embedding materials into fiber matrices to enhance their thermal properties.nbsp; Silica aerogel was embedded into an alumina fiber matrix to create Flexible Insulation with a Reinforced Aerogel (FIRA).nbsp; In the current Phase I effort, a High Temperature FIRA (HTFIRA) will be demonstrated by embedding aerogel with a higher temperature capability.nbsp; Since commercially availablenbsp;aerogel blankets are currently limited to 1200OF, producing HTFIRA with a scalable manufacturing process would be a significant advance in the state-of-the-art.nbsp; The re-entry trajectory and payload capacity of Hypersonic Inflatable Aerodynamic Decelerators (HIADs) arenbsp;limited by the materials in the Thermal Protection System (TPS). nbsp;For example, the TPS on the LOFTID (Low-Earth Orbit Flight Test of an Inflatable Decelerator) uses carbon felt and silica aerogel that degrade during re-entry when temperatures can exceed 2800OF.nbsp; Replacing all or part of these layers with HTFIRA will allow higher heating rates without degradation, facilitating heavier payloads and more direct re-entry trajectories.nbsp; HTFIRA will also be more flexible, lighter and more compact than the existing TPS materials, further increasing the payload capacity of HIAD.nbsp; In Phase I, SDMA will collaborate with NASA Glenn Research Center to make aerogel.nbsp; SDMA will then embed that aerogel in an alumina fiber matrix to demonstrate HTFIRA.nbsp; nbsp;Thermal properties will be determined.nbsp; In a parallel effort in preparation for Phase II and III, SDMA will investigate the scalability of the aerogel manufacturing process and the compatibility of HTFIRA with the fabrication methods developed for the TPS of LOFTID.nbsp; HTFIRA promises a significant improvement in TPS for multiple Entry, Descent and Landing (EDL) strategies including HIAD and controlled flight through planetary atmospheres.

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