SBIR/STTR Research Award
Seam Joining Techniques for Three-Dimensional Woven Carbon Naterial of at Least 1" Thickness.
Award amount
$102,203Program and phase
SBIR · Phase IAward year
2014Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- Pham, Tuyetnhung
- Proposal award date
- 2014-06-20
- Contract end date
- 2014-12-19
- UEI
- Not reported
- Solicitation number
- Not reported
- Topic code
- H7.01
Research abstract
Heat shield technology is a critical component for both re-entry and
hypersonic vehicles. The traditional manufacturing approach for
designing heat shields consists of joining TPS tiles together with an
adhesive that fills any gaps between them. This approach has significant
challenges, including the reduction in thermal-mechanical performance as
compared to that of acreage woven material. Nhung's Notions proposes to
address this problem by modifying existing equipment to mechanically
join these materials prior to infusion. In Phase I, we will determine
the material and pattern parameters required to use with equipment to
prepare the joins while minimizing damage to the pristine woven material
while maintaining consistent thickness between pre- and post- joined
material keeping pattern consistency throughout the process.
Technology keywords
Not reported
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
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- Heat Shield Recession Measurements Using Remote Spectral Sensors